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NOTE: The Solicitations and topics listed on this site are copies from the various SBIR agency solicitations and are not necessarily the latest and most blackjack camo stencils />For this reason, you should use the agency link listed below which will take you directly to the appropriate agency server where you can read the official version of this solicitation and download the appropriate forms and rules.
The official link for this solicitation is: TECHNOLOGY AREA S : Air Platform OBJECTIVE: The key objective of this work is to evaluate the mechanical properties and microstructural characteristics of post-process heat treatments of Additively Manufactured AM Ti-6Al-4V alloy including process-structure-property relationships.
Tensile testing, smooth bar high cycle fatigue testing and microstructural analyses are to be performed on Laser Powder Bed Fusion L-PBF manufactured near net shape Ti-6Al-4V specimens having four heat treatment types after Hot Isostatic Pressing HIP.
These heat treatments are Mill-Anneal MAANNeal ANNSolution Treat and Age STA just click for source Beta Solution Treat and Overaged BSOA.
The resulting mechanical properties and microstructures will be compared to the traditional Ti-6Al-4V alloys bars, forgings and castings.
The quantitative process-structure-property relationships will be determined with computational modeling with respect to build orientation.
DESCRIPTION: Additive Manufacturing AM is a new production technology that enables reduced manufacturing steps, part consolidation and production of near net shape parts from 3-D model data.
Current applications mainly focus on secondary structures or other non-critical applications.
Recent developments in AM technology and Https://chicago-lawyer.info/blackjack/blackjack-new-york.html Standards offer great potential to implement AM produced part in the US Army.
The use of AM titanium alloy replacement of a currently used traditional titanium alloy in the US Army helicopters with a same traditional alloy heat treatment types may not provide an increased utilization of the AM titanium alloy and may cause additional performance risk since heat treatment for AM titanium alloy is not optimized.
The thickness of the part affects the grain size of the part during solidification as such the grain sizes are smaller for the small thickness compared to the thick part.
Therefore, tensile properties are higher for a part with small grains even though both part had same heat treatment types.
On the other hand, the tensile properties are also depends on heat treatment types.
For example, annealing heat treatment provides lower tensile properties compared to the solution heat and aged heat treatment.
Therefore, the effects of heat treatment types coupled with part thickness and resulting mechanical properties need to be thoroughly investigated.
In this study, the L-PBF AM process will be used to manufacture near net shape AM Ti-6Al-4V test specimens, and evaluate the effect of post-processing heat treatment types on tensile and fatigue properties, compared to the baseline Ti-6Al-4V alloy bar, forging and casting material properties.
To understand the process-structure-property relationships, computational modeling is to be utilized to predict the quantitative mechanical properties such as tensile, yield, elongation and fatigue strength.
The project will be conducted in three phases.
Phase I will focus on assessment, design and selection of parameters, computational model, manufacturing options and procurement of AM Ti-6Al-4V alloy powder.
Phase II will focus on demonstrating the ability to manufacture near net-shape of tensile and fatigue specimens, perform tensile, fatigue tests and evaluate tensile, fatigue test results of four heat treatment types MA, ANN, STA and BSTOA and quantitative prediction of process-structure-property relationships along different directions.
Ten tests 10 at room temperature per heat treatment types will be evaluated for both tensile and high cycle fatigue 0.
Beta transus temperature of the two specimens will be determined for heat treating guidance.
The chemical composition and density of the each lot will be determined.
The chemical composition and physical properties of the Luxor $5 blackjack powder will be verified.
Only one batch of virgin powder and no recycled powder will be used.
A few trial manufacturing is to be made to verify specimen sizes, quality and tensile properties.
Phase III will focus introduction of AM Ti-6Al-4V alloy into a broad range of defense and civilian applications.
This technology has been demonstrated in a laboratory research scale and prototype parts.
The current effort would use existing technology to develop an optimized heat treatment types for AM Ti-6Al-4V alloy process utilizing simple shaped tensile and fatigue specimens.
PHASE I: Wizard of odds blackjack variants One evaluates click at this page engineering merit and feasibility of the proposed technology.
It identifies and builds team with industrial partners, design and select AM Ti-6Al-4V powder type, size and amount of experimental test specimens, AM manufacturing and, assesses application and manufacturing options, addresses producibility and inspectibility using these test specimens, selects predictive computer modeling and investigates the overall benefits of the project.
The interrelations among AM processed Ti-6Al-4V alloy heat treating conditions and resulting microstructure parameters alpha layer thickness, alpha and beta phase content, grain size, density, etc.
To understand the process-structure-property relationships computational modeling need to be utilized to predict the quantitative mechanical properties.
The objective of the process-structure-property relationships between the heat treating conditions and microstructural features is to be able to predict the microstructure and resulting mechanical properties for a given part geometry, size, and feature orientations for a given heat treating conditions.
Such a model would be the basis for improving first part yield and enabling rapid part qualification.
In order to verify the process-structure-property https://chicago-lawyer.info/blackjack/live-blackjack-dealers-online.html, experimentally measured microstructural features and tensile properties are required in x, y and z directions.
A generic computational model or a modified one to predict properties could be used for predicting process-structure-property relationships.
To predict a complex part process-structure-property relationships, selected complex shaped parts will be modeled to determine properties.
These https://chicago-lawyer.info/blackjack/increase-odds-in-blackjack.html complex shaped parts will be manufactured in Phase II and mechanical properties and microstuctural features will be measured with respect specimen orientations for modeling verification.
Recommended computational modeling is to be demonstrated with open source microstructure and mechanical data for the AM Ti-6Al-4V alloy.
Further ideas beyond described are welcome.
An appropriate process modeling could be used to minimize process defects and maximize the mechanical properties for optimum producibility if needed and funding are available.
Required Phase I deliverables include monthly progress reports, final technical report including specimen sizes, testing specimens locations, tests, powder specification and amount, AM build layout and manufacturing plans, predicted computational model examples demonstrating the process-structure-property relationships including complex shapes.
PHASE II: Phase Two will manufacture the specimens and evaluate tensile and fatigue test results, predictive computational modeling compared to the traditional Ti-6Al-4V alloy bars, forgings and castings.
The process will utilize an L-PBF process.
The shapes of AM specimens will be simple-shaped L-PBF manufacturing.
The overall dimension in length could be 8.
Any required radiuses could be 0.
All specimens will undergo HIP prior to the following heat treatments: 1 mill-anneal, 2 anneal, 3 solution treated and age and finally 4 beta solution treated and overaged.
Tensile, fatigue, hardness, density, optical microscopy, scanning electron microscopy and computer tomography CT analyses are to be utilized to generate and analyze the resulting data during the Phase II effort.
Ten 10 tests will be performed at room temperature per heat treatment types.
Additionally, ten 10 tests will be performed at room temperature as AM manufactured and as HIPed for baseline comparison.
Tensile, fatigue, hardness, density, optical microscopy, scanning electron microscopy and computer tomography CT analyses are to be utilized to generate and analyze the resulting data during the Phase II tensile evaluation.
The specimens will undergo both tensile and high cycle fatigue 0.
Beta transus temperature of the two specimens as well as the chemical composition of each lot will be determined for heat treating guidance.
Additionally, the chemical composition and physical properties of the Ti-6Al-4V powder will also be verified.
Only one batch of virgin powder no recycled powder will be used, and all specimens will come from the same AM build feedstock.
Trial printed specimens will be made to verify specimen sizes, quality and tensile properties.
The interrelations among AM processed Ti-6Al-4V alloy heat treating conditions and resulting microstructure parameters alpha layer thickness, alpha and beta phase content, grain size, density, etc.
To understand the process-structure-property relationships, computational modeling is to be utilized to predict the quantitative mechanical properties.
Such a model would be the basis for improving first part yield and enabling rapid part qualification.
In order to verify the model, experimentally measured microstructural features and tensile properties are required in x, y and z directions.
The resulting data is to be used to validate the computational modeling.
Required Phase II deliverables include bi-monthly progress reports, test reports, computational predictive mechanical property evaluation and a final technical report including powder chemical and physical properties, AM Ti-6Al-4V chemical analysis, CT and dimensional inspections, tensile, hardness, fatigue testing, microstructure, fractography analysis, computational model inputs to predict properties, verification and example of the model predictions.
PHASE III: Phase Three will address the transition path of this technology resulting from Phase II effort to various US Army components with industrial partners and Original Equipment Manufacturers OEMs.
This technology has been demonstrated in a laboratory research scale and on prototype parts.
This program effort would use existing technology to develop an optimized heat treatment process for AM Ti-6Al-4V alloys, quantitative process-structure-property relationships utilizing simple shaped tensile and fatigue specimens.
The implementation targets are defense applications.
The expected benefit of the resulting project data could become a heat treatment guide for AM Ti-6Al-4V alloy components used in US Army applications requiring tensile strength, fatigue strength and combination of both tensile and fatigue strength for performance requirements.
The relevant technical data generated and experience gained in this project are expected to positively impact application of additively manufactured titanium components in a broad range of defense applications where light weight and reduced lead time are needed for very complex parts that use titanium components.
All these project benefits will results in improved U.
REFERENCES: 1: Seifi, M.
Overview of Materials Qualification Needs for Metal Additive Manufacturing.
JOM, 2016, 68, 747—764.
Effects of processing parameters on microstructure and mechanical property of selective laser melted Ti6Al4V.
As-Fabricated and Heat-Treated Microstructures of the Ti-6Al-4V Alloy Processed by Selective Laser Melting.
A, 2011, 42, 3190—3199.
High density Ti-6Al-4V via SLM processing: Microstructure and mechanical properties.
In Proceeding of the 22nd Annual International Solid Freeform Fabrication Symposium, Austin, TX, USA, 8—10 August 2011, 475—483.
On the mechanical behaviour of titanium alloy TiAl6V4 manufactured by selective laser melting: Fatigue resistance and crack growth performance.
Fatigue, 2013, 48, 300—307.
KEYWORDS: Additive Manufacturing, Heat Treatment, Ti-6Al-4V Alloy, Tensile Properties, Https://chicago-lawyer.info/blackjack/how-to-deal-in-blackjack.html, Laser, Powder Bed Fusion, Process Structure Property Relationships TECHNOLOGY AREA S : Info Systems OBJECTIVE: Cybersecurity systems need to take advantage of high assurance provided by state machines used for aviation and safety critical systems.
Offeror shall research a high assurance state machine trusted computing base for a high assurance operating system.
DESCRIPTION: Safety critical systems use state machines to achieve high computer security assurance levels.
State machines make security reviews for EAL6 or higher tractable.
Current generation aviation systems were not developed with strong computer security requirements.
Embedded system designs are typically based on commodity hardware optimized exclusively for speed — leading to critical cyber vulnerabilities that can have devastating effects on safety and mission effectiveness.
We are interested in researching a separation kernel-like operating system consisting of a hardware state machine as the trusted computing base and a high assurance operating system.
In terms of computer virtualization concepts: the trusted computing base is a hardware state machine and the OS can be compared to a guest operating system.
Open source architectures also provide for lower life cycle system cost.
We are interested in leveraging the open source communities for this research topic area.
Preference will be given for open source hardware and operating system modules.
PHASE I: For the Phase I proposal, offeror blackjack trainer online game describe the feasibility of using a hardware and software co-design to create a high assurance state machine as the trusted computing base for a high assurance operating system.
For the phase I effort, the offeror shall demonstrate the feasibility and security benefits of creating a high assurance hardware state machine trusted computing base and high assurance OS.
It is highly recommended that the offeror team with a government prime contractor.
The Offer shall propose potential applications for a system demonstration and implement an application with government concurrence.
Offeror shall deliver a year 1 report and a year 2 report describing artifacts, documents, verification tests, etc.
Offeror shall deliver 2 prototype systems to the government point of contact for test and evaluation with all software tools and licenses if required to build and use the system.
Offeror shall provide 2 days of on-site training for the system.
PHASE III: Offeror will develop and market high assurance system based on phase II development work and marketing plan from phase I.
Offeror will achieve EAL6 or greater for high assurance computer system.
Fannon: An analysis of hardware-assisted virtual machine based rootkits, Thesis, Naval Postgraduate School, June 2014.
SPIE 10652, Disruptive Technologies in Information Sciences, 106520P 9 May 2024 11: doi: 10.
Nakano: "Hardware Implementation of a Real-time Operating System," IEEE TRON Project International Symposium, Tokyo, Japan, pp.
DESCRIPTION: Emerging aircraft concepts are calling for increased electrical power and in many cases all electric aircraft designs.
While accommodating the electric power requirement is a challenge in and of itself, thermal management of the components for the system becomes a priority engineering challenge as well.
From a military perspective high pulse power loads devices, such as DEWs, offer significant opportunities, as well as challenges, compared to traditional kinetic weapons.
Airborne DEWs could perform a variety of Army missions including missile defense, counter-UAV operations, suppression of enemy air defenses, precision strike, etc.
Although not limited to high energy lasers HELsthe challenge of integrating such a device into a mission equipment package MEP illustrates the technical challenges ahead.
HELs do not consume ammunition in the traditional sense, though they do consume significant amounts of electrical power.
This means that to fire a 50 kW laser, 100 kW of electrical power would be needed.
In addition, the net 50 kW of waste heat that is rejected to fire the laser must also be cooled which requires a cooling device that adds more size, weight, and power SWaP.
Additionally, operating temperatures of the device are close to the operating temperatures of the external ambient air.
The low quality heat is extremely difficult to move around.
Therefore, significant incentive exists to maximize the efficiency of airborne DEWs to minimize both power and thermal management requirements.
One way to enhance the efficiency of a laser is to cool it and operate the laser at cryogenic temperatures.
Research has shown that wall-plug efficiency in excess of 70% is possible for cryogenically cooled solid-state lasers using liquid nitrogen LN2.
An airborne DEW operating at this efficiency would have significantly reduced power and thermal management requirements, but these benefits are only possible if the system is cryogenically cooled.
For a cryogenic cooling system to be attractive, the benefits of increased efficiency must outweigh the cost, complexity and SWaP penalties associated with its implementation.
Metric goals and characteristics for the on-wing cryogenic liquid generator are as follows.
Weight of the production equipment should not exceed 250 kg; weight is highly valued on a rotorcraft, hence any that can be removed should be.
Operational ceiling is what blackjack contracts to 5500 meters; performance must be characterized over the operational range.
Temperatures up to 50 Blackjack 21 casino should be considered.
If bleed air from an aircraft engine or secondary power unit SPU is required in the design, limit the bleed flow to a maximum.
Electrical power to drive equipment can assume 270VDC and an allotment of up to 40 kW of electrical load.
Note, this system is not limited to LN2, innovative concepts which use any low temp fluid will be considered, such as, but not limited to liquefied natural gas LNGAmmonia, liquid ethylene, etc.
PHASE I: Develop a design for a cryogenic liquid generator which meets or exceeds the aforementioned specifications.
Utilization of models, and a systems engineering perspective is encouraged.
PHASE III: Phase III options would include development of a fully-functional prototype that could be used for cryogenic DEW ground and flight testing.
For dual us applications the same technology could also be applied for other ground, naval, and airborne thermal management applications such as cooling superconducting systems including high-efficiency, compact motors and generators and lightweight power distribution systems.
Paschotta, article on 'cryogenic lasers' in the Encyclopedia of Laser Physics and Technology, 1.
Edition October 2008, Wiley-VCH, ISBN 978-3-527-40828-3 3: Rodger W.
Dyson, "Novel Thermal Energy Conversion Technologies for Advanced Electric Air Vehicles" 4: Scheidler, Justin J.
AIAA Propulsion and Energy Forum.
Army Weapons-Related Directed Energy DE Programs: Background and Potential Issues for Congress", Congressional research Service Report R45098 2018.
KEYWORDS: Directed Energy Weapons, Auxiliary Power Unit, Thermal Management, Cryogenic Cooling TECHNOLOGY AREA S : Weapons OBJECTIVE: Develop novel muzzle brake structures for extended range cannon artillery systems that reduce mass and manufacturing cost, while maintaining or improving recoil reduction, signature management, durability, and operator safety.
These include but are not limited by munitions currently under development for direct and indirect fire missions.
High pressure produced at muzzle exit have negative impact upon the surrounding environment due to muzzle blast flow fields exiting the barrel.
The negative consequences, such as recoil and noise production, can be alleviated by redirecting propellant gases.
Muzzle brakes have been used for decades to efficiently redirect propellant gas, resulting in effective performance gains.
However, recent advances in materials and additive manufacturing techniques show promise for muzzle brake weight reduction and manufacturing cost while maintaining the favorable flow field response and resistance to the resulting thermal and pressure loading.
Muzzle brakes are subject to what is exposure blackjack loading due to high exit pressure and gas momentum from the projectile emersion from the gun tube.
Conditions at muzzle exit are dynamic and vary based on multiple factors.
Typical pressure and thermal conditions have been found to be as much as 10-12 ksi and 2000 K, respectively.
The muzzle environment can cause erosion on the brake surfaces.
The shape of the muzzle brakes often consists of complex three dimensional curves and multiple openings.
Examples of various muzzle brakes over the last century can be found in the references.
This topic seeks to develop novel applications of advanced materials, coatings and manufacturing technologies to muzzle brakes.
A variety of analyses and tests should be done to show that the materials can survive the environment and that the manufacturing process can produce the complex shapes required.
The objective for this effort is to achieve 30 percent weight reduction with either comparable or reduced cost compared to conventional steel muzzle brakes.
PHASE I: Evaluate various material and coating combinations for use in the muzzle brake environment.
Investigate manufacturing technologies such as additive manufacturing for combination with promising materials and coatings.
Reference 1 AMCP 706-251section 3-3.
Conduct an analysis of alternatives to select the best combination of materials and manufacturing for prototypes to be delivered in Phase II.
Select a candidate shape for Phase II.
Reference 4 US Patent No 8,424,440 for a 105mm gun is the preferred shape but other 105mm or 155mm shapes may be used with TPOC concurrence.
Perform a preliminary validation of the manufacturing concept, and prepare initial production cost estimates for the designs under consideration.
Perform feasibility trials on the production of the muzzle brake design selected in Phase I.
Perform final design refinements.
Document final material, coating, and manufacturing process.
PHASE III: Conduct a live fire demonstration of the final prototype in an operational environment with involvement from the prime contractor for the weapon system.
Explore potential small arms applications for both military and private sector customers.
REFERENCES: 1: Headquarters, U.
Ballistics: Theory and Design and Ammunition.
Contribution to the Analysis of Muzzle Brake Design.
ROCK ISLAND ARSENAL IL, 1962.
KEYWORDS: Muzzle Device, Muzzle Brake, Manufacturing, Artillery, Cannon TECHNOLOGY AREA S : Weapons OBJECTIVE: Develop a system to aggregate friendly force small arms fire control data to compute and display which individual or team has the highest probability of successfully engaging a target.
DESCRIPTION: This effort supports the Army Modernization Priority of Soldier Lethality.
Smart, networked small arms fire control systems are increasingly commonplace, especially with the proliferation of smartphones.
These capabilities allow users to quickly create and edit ballistic inputs to maximize effects.
These techniques allow a user to provide a performance estimate for a weapon system given its ballistic parameters and the user's ability to measure and control the other factors that affect the flight of a bullet.
By developing a method to connect the fire control systems to a centralized probability of hit calculator, this topic seeks to provide unit commanders with the capability to determine which asset at his disposal e.
This would not be based only on user-provided information but would tie in actual measurements from sensors like weather meters, laser rangefinders, and weapon-mounted displays.
This data will provide the most accurate picture of friendly units' ability to engage threats.
The integration of this data would enable a commander to evaluate the impact of moving units and threats around on a map, and to evaluate how the firing solutions and P hit calculations change, allowing him to determine which unit should engage each target to maximize the probability of successfully neutralizing the enemy.
PHASE I: The objective of Phase I is to develop a system architecture and methodology for aggregating fire control data over a generic network that enables the data to be transferred and shared among systems.
Document the proposed solution.
Demonstrate software that couples simulated data from multiple sources with target profiles to compute a firing solution and probability of hit for each friendly asset.
PHASE II: Phase II will build on a successful Phase I demonstration to connect physical devices to the probability of hit application and develop a user interface that presents the information on a map.
The map should factor local terrain into the firing solution.
The application should allow the input of enemy locations from users or from other sources.
Demonstrate the capability to concurrently connect over 50 devices to the network and display their computed performance probabilities based upon the entered enemy parameters.
PHASE III: This technology can be provided to law enforcement to help in deployment of their units in counter-sniper applications.
https://chicago-lawyer.info/blackjack/uk-online-blackjack.html capability could be extended to other types of munitions, such as vehicle mounted weapons or indirect fire weapons, to help commanders better plan positioning of the units.
There is also the potential for this capability to be used in the commercial market, allowing hunters to determine the best place to sands regency blackjack up for engaging targets.
Chen, "Research on multi-sensor data fusion technology based on PSO-RBF neural network," 2015 IEEE Advanced Information Unexpectedness! blackjack skip beat assured, Electronic and Automation Control Conference IAEACChongqing, 2015, pp.
These composites are used on large caliber direct and indirect fire gun tubes.
They use polyetheretherketone PEEK as the thermoplastic matrix and are processed via fiber placement.
The increase in the through thickness modulus should not decrease the in-plane properties of the composite nor the ability to process it via fiber placement.
DESCRIPTION: There is a need to increase the through thickness modulus in fiber placed thermoplastic composites.
These materials are being used to overwrap gun tubes for both direct and indirect fire and the effectiveness of the composite wrap is limited by the through thickness modulus.
Traditionally this modulus is only that of the matrix material which is an order of magnitude or more lower than that of the reinforcement.
On previous efforts it was found that after about 0.
This effort focuses on developing a process to increase the through thickness modulus by adding nano-materials to the matrix.
The addition of these materials should not be detrimental to the in plane properties of the base composite and should still be processable via fiber placement.
PHASE I: Develop a process to increase the through thickness modulus of carbon fiber reinforced thermoplastic by adding nano-materials to the system.
This material is processed via fiber placement using either hot please click for source torches or lasers as the heating source.
A suggested method for measuring the through thickness modulus is ASTM D695 with two to one size anisotropy though other methods are acceptable.
The threshold is a 75% increase in through thickness modulus over the baseline of pure PEEK.
The objective is a 200% increase.
The material deliverable is the equivalent of one square meter can be of any width of the improved material for testing.
The material deliverable does not have to be in a form processable by fiber placement but should be processable by heated platen press or autoclave.
PHASE II: Refine the process and improve the modulus results over Phase I.
Minimum expected improvement is 100% over pure PEEK with an objective of 200% or more increase.
Material must be processable via fiber placement.
The as processed interlaminar shear strength D2344 -Standard Test Method for Short-Beam Strength of Polymer Matrix Composite Materials and Their Laminatesshall be equal to or greater than 9 ksi and any deviation from this value shall be reported and a plan to achieve 9 ksi shall be described.
No degradation of the in-plane properties shall be verified by conducting at a minimum ASTM D3039 Standard Test Method almost atlantic city blackjack rules Tensile Properties of Polymer Matrix Composite Materials in both longitudinal and transverse directions.
Thermal conductivity shall also be measured to determine if there is any increase over the baseline material.
PHASE III: Finalize the development of a material based solution at production level quantities that can be readily implemented on existing manufacturing equipment.
Non-DoD applications include down well piping, engine components, etc.
Littlefield, Minimizing Rail Deflections in an EM Railgun, November 2006.
Studart, "Composites Reinforced in Three Dimensions by Using Low Magnetic Fields," Science, Vol 335, 13 Jan 2012, pp 199-204 3: L.
Troiano, Army Targets Age Old Problems with New Gun Barrel Materials, AMPTIAC Quarterly, v8n4, 2004.
Hyland, Prestressed Carbon Fiber Composite Overwrapped Gun Tube, November 2006.
Ellis, Large Caliber Gun Tube Materials Systems Design, 10th U.
Army Gun Dynamics Symposium Proceedings, Austin, TX, April 2002.
Army Materiel Command, "Research and Development of Materiel, Engineering Design Handbook, Gun Series, Gun Tubes," AMCP 706-252, Washington DC 1964.
Koratkar, "Observation of High Buckling Stability in Carbon Nanotube Composites", Advanced Materials, Vol 18, 4, 2006, 452-456.
Koratkar, "Enhanced Mechanical Properties of Nanocomposites at Low Graphene Content", ACS Nano, 3 122009, 2884-3890 11: M.
Koratkar, "Enhanced Mechanical Properties of Nanocomposites at Low Graphene Content", ACS Nano, 3 122009, 2884-3890 KEYWORDS: Advanced Composites, Nanomaterials, Fiber Placement, Thermoplastic Composites TECHNOLOGY AREA S : Electronics OBJECTIVE: Investigate and develop innovative solutions to enable integration of electronic warfare antennas on munition launched rounds.
Antenna systems must be capable of surviving a typical mortar gun launch and maintaining their operational performance throughout flight.
DESCRIPTION: Recent advancements in high-shock, munition-launched compatible electronics technology particularly have opened up a wide realm of possibilities for enabling long-range and inexpensive electronic warfare attacks of ground targets via relatively inexpensive munition launched systems and projectiles.
To enable this mission, projectiles must be equipped the associated electronics and RF sensors.
Due to the highly constrained volume and structural integrity requirements, these sensors must be conformal to the outer mold line with very minimal intrusion into the structural wall of the projectile.
Surface area on these projectiles is also very limited; therefore, these sensors must be small, residing within the allotted payload space.
It is also requisite that the sensor operates over several ISM bands, while providing omni-directional beam pattern coverage.
Army is looking for novel advancements in conformal antenna technology to enable this mission set on a range of prospective gun-launched platforms e.
Aperture designs should be innately scalable to accommodate different munitions with tuneable frequency characteristics and incorporate knowledge and understanding of relevant high-shock compatible materials and construction techniques.
A critical aspect of the effort involves that the apertures are insensitive to large changes in response due to the large shock loads experienced during launch.
Furthermore, designs should incorporate knowledge and understanding of miniaturization techniques, while still achieving the objective bandwidth and pattern coverage requirements.
PHASE I: During the Phase I contract, successful proposers shall conduct a proof of concept study that focuses on the feasibility of designing the antenna apertures.
Investigations should include analysis of potential aperture mounting configurations, achievable antenna performance gain, bandwidth, pattern coverageand materials capable of surviving the expected https://chicago-lawyer.info/blackjack/5-card-trick-blackjack.html />Verification of RF performance shall be accomplished through simulation and prototype antenna measurements.
A final proposed concept design, including a detailed description and analysis of both expected thermal and mechanical loads, is expected at the completion of the Phase I effort.
PHASE II: If selected for a Phase II, the proposer shall fabricate and integrate the prototype antenna apertures into a nominal projectile form-factor.
Special emphasis on launch survivability will be required, including hard force and electromagnetic effects during testing to ensure the apertures can avoid failure or degradation.
Information and data collected from the flights will be used to validate operational electrical performance.
PHASE III: Phase III selections shall ruggedized final design, fabricate it and integrate the prototype antenna apertures into nominal projectile form-factor to be identified by the Government.
Phase III selections might have adequate support from an Army prime or industry transition partner identified during earlier phases of the program.
Further commercial applications include civilian space-flight initiatives and application of the antenna technology for the design of low-cost, high-temperature, high-shock antenna sensors.
REFERENCES: 1: Grzybowski, David M.
Peregino, and Bradford S.
Development of a Telemetry-Enabled High-G Projectile Carrier.
ARMY RESEARCH LAB ABERDEEN PROVING GROUND MD WEAPONS AND MATERIALS RESEARCH DIRECTORATE, 2012.
DESCRIPTION: This effort aims to provide a significant capability to the Soldier Lethality CFT by increasing data accuracy during the direct fire engagement process for digital soldiers.
Current technologies should allow the development an optimized solution to cover a predetermined area of interest by the swarms of combined assets in the persistent way.
In particular, this coverage will involve both mobile and stationary target acquisition and engagement assets.
Some of these assets may be weaponized to engage the targets.
The route patterns of moving assets can be assumed to be fixed in order to satisfy the persistent surveillance requirement.
For stationary assets, the maintenance requirements may be significantly relaxed since the power consumption of these assets can be significantly reduced.
These assets might geolocate the targets and serve as potential forward observers for engaging the targets.
The optimized solution should rely as much as possible on autonomy to enable assets capable to return to their place s of origin on with minimal communication both among assets with the operator unit controller OUC.
Special attention should also be paid to assure the collision avoidance among assets.
PHASE I: Design and develop innovative state-of-the-art software optimization algorithm for the persistent coverage of a predetermined area of interest by the swarms of assets capable of autonomous navigation.
Demonstrate how the proposed algorithms will optimize the coverage provided by assets in a dynamic threat environment.
PHASE II: Develop and demonstrate a prototype capability with swarms of at least six assets autonomously navigating over a predetermined area of interest using the developmental offline software algorithms.
The collaborative assets should be demonstrate the capability of autonomous return to their points of origin.
This prototype should be capable of integrating with CCDC Armaments Center supplied fires and effects architecture.
Conduct testing to demonstrate feasibility of this technology for operation within a simulation environment operated by CCDC Armaments Center.
Department of Homeland security could use this capability to monitor the illegal crossings of the US borders.
Bogdanowicz, "Swarm of autonomous unmanned aerial vehicles with 3D learn more here, Proc.
Bogdanowicz, "Flying swarm of drones over circulant digraph", IEEE Transactions on Aerospace and Electronic Systems, Vol.
Chen, "An overview of recent progress in the study of distributed multiagent coordination", IEEE Transactions on Industrial Informatics, Vol.
Zhang, "How much control is enough for network connectivity preservation and collision avoidance?
Karatas, "Single-view distance-estimation-based formation control of robotic swarms", IEEE Transactions on Industrial Electronics, Vol.
Ahn, "Formation coordination for propagation of group of mobile agents via self-mobile localization", IEEE Systems Journal, Vol.
DESCRIPTION: With the evolution of modern battlefields, the Army is seeking a new generation of munitions to overmatch, deter and disrupt its adversaries.
The next-generation of weapons aims to provide an increased kinetic advantage over increasingly complex targets, situations and at longer distances.
The increased complexity of munitions, where target identification and guidance systems now occupy a larger portion of the warhead, has been made at the expense of the payload.
The integration of reactive materials has been identified and demonstrated as a method to restore lethality by increasing the overall energy output of these enhanced munitions and improving system effectiveness.
However, the integration of these materials has been limited by their mechanical properties.
This topic aims at further expanding the field of structural reactive materials SRMwhere a portion of the traditional ordnance is replaced with an SRM.
Such multi-purpose components offer opportunities to integrate materials of high strength and density that adds additional damage mechanism to defeat the target.
The objective of this program is to develop novel SRMs with mechanical properties and density similar or superior to munition-grade read article, and capable of providing an energetic output upon initiation by detonation or high-velocity impact, while maintaining their integrity under the harsh launch conditions and flight loads resulting from the next-generation guns.
Focus should also be given to the establishment of novel processing methods to ensure the rapid transition of the proposed technology into new or existing weapon systems.
This proposal shall develop and demonstrate the properties of these multifunctional materials in comparison with established inert materials.
The characterization will include mechanical properties such as tensile and compression strength, density and hardness.
The energetic performance of the novel SRM will be characterized by experimental testing to measure energy release and warhead fragmentation PHASE I: Develop at least one novel SRM with a density equivalent or superior to munition-grade steel.
Perform characterization experiments to establish the mechanical, thermal and energetic performance of the SRM in comparison with baseline inert material such as munitions grade steel.
Conduct small scale fabrication to show manufacturing feasibility.
Provide material sample to the Army POC.
PHASE II: Further develop and optimize the SRM established in Phase I using thermodynamic analysis to achieve the best combinations of mechanical and energy release properties.
Measure energy release and characterize warhead case fragmentation in small scale tests, such as blast chamber testing.
Scale-up the manufacturing process and produce prototypes in at least 3 configurations of interest to the Army and deliver 5 prototypes from each configuration to the Army.
PHASE III: Transition the developed materials and related technology to a major manufacturer for incorporating this technology into next-generation munitions for the long range precision fire LRPF program.
To further exploit the benefits of the developed technology, form partnerships with other manufacturers for applications to the civil sectors, such as the oil well and construction industries.
This technology can also be leveraged to mining applications as well as applications occur in submarine blasting, breaking log jams, breaking ice jams, initiating avalanches, timber or tree cutting, the perforation of arctic sea-ice or permafrost, glacier blasting, ice breaking, and underwater demolition.
Pham, Processing and Handling of Reactive and Structural Reactive Materials, AIChE Annual Meeting, 2009.
Hanagud, Preliminary design of multifunctional structural-energetic materials for high density, high strength and release of high enthalpic energy, International Journal of Scientific Engineering and Technology 3 2014 1189-1192.
DESCRIPTION: Energetic material advances have resulted in the development of several suitable lead-free replacements for lead styphnate and lead azide in munition formulations.
These lead-free energetic materials could potentially create unexpected corrosive environments for traditional cartridge brass and other munition components.
Field https://chicago-lawyer.info/blackjack/rtg-blackjack-strategy.html of ammunition components is therefore critical in future deployments to assure weapon system effectiveness from the ammunition life cycle perspective, i.
Many field techniques are currently subject to a visual inspection of the small arms ammunition but recent advances in non-destructive metallurgical and material analysis allows for this inspection to be more analytically robust and time effective.
This SBIR project provides the opportunity to employ these modern corrosion inspection techniques to be implemented for use in developmental stages of new energetic materials and in the field for a wide range of small arms ammunition components.
PHASE I: Develop process validity and methodology for non-destructive inspection of modern explosives and munition housings on a lab scale.
Identify, develop, and test likely lead-replacement candidates against likely substrates based on the published literature.
Major considerations for the success of the feasibility study include the time of inspection and quality of the reported data.
PHASE II: Based on the methodology established during the Phase I, a hand-held test cell prototype will be developed and certified to the appropriate Military standards, specifications, and UL requirements.
This prototype test cell will incorporate appropriately designed small arms ammunition component tooling to provide an interface with different applications.
A working prototype test cell with directions on its use will be delivered to the Program Executive Officer for Ammunition for field testing.
PHASE III: If this program is demonstrated to be successful, this non-destructive inspection technique for modern explosives and ammunition housings can be used in both military and civilian applications.
Military applications include small arms components 5.
Civilian applications include hunting, sport shooting, and law enforcement.
REFERENCES: 1: Military Standard Practice MIL-STD-889C, Dissimilar Metals, revision C DOD, 22 August 2023 2: Design Criteria Standard MIL-STD-1568C, Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems, revision C DOD, 12 August 2023 3: Test Method Standard MIL-STD-1904B, Design and Test Requirements for Level A Ammunition Packaging, revision B, DOD, 09 March 2024 4: Drobockyi, Volodymyr and Viggiano, Anthony, inventor 5: Shell Shock Technologies, Inc.
Dezincification of Cartridge Brass.
Sintox — A New, Non-Toxic Primer Composition by Dynamit Nobel AG.
Nano Energetics for US Navy Percussion Primer Applications.
San Francisco, CA 9: Fischer D.
Angewadnte Communications, International Edition.
DBX-1 - A Lead Free Replacement blackjack count Lead Azide.
Once a proof-of-concept optical design is demonstrated, a cost model should be established, as well as a transition plan to bring the sensors into production.
Emphasis during all phases of this project should be on developing a sensor with minimized cost and size.
DESCRIPTION: Most current fielded proximity sensor today are RF based.
With the increasingly cluttered RF environments, the need for different proximity sensor base technologies has been realized.
Standoff distances anywhere from 0.
PHASE I: During Phase I, a feasibility study of the proposed sensor concept shall be conducted to provide evidence that demonstrates the concept can meet the stated requirements.
This study should identify the equipment and resources needed to prototype a device, as well as initial device designs and unit cost estimates.
PHASE II: Phase II shall begin by prototyping the initial sensor design and evaluating its performance against the stated requirements.
It is expected that one or more design iterations will occur during the 2nd phase.
Phase II will end with a proof-of-concept prototype that demonstrates the performance and producibility of the sensor through a gun fired test.
Deliverables include quarterly progress reports, prototype hardware, a manufacturing plan, a field test and a final report.
PHASE III: Phase III shall begin with the execution of the manufacturing plan developed in phase II.
Continued development of the sensor shall be pursued to reduce manufacturing costs.
Key military applications for these devices are for end game fuzing.
This technology can be expanded to commercial applications including car safety awareness systems.
DESCRIPTION: The US Army is in need of weight reduction for components used in gun-launched environments.
In order to achieve the desired online blackjack instant player edge reduction, manufacturing processes other than the traditional subtractive types need to be explored.
This project will investigate innovative materials, designs, and manufacturing methods to minimize production cost, minimize weight, and maintain the relevant performance requirements.
Components can vary in both size and shape with a volume not to exceed 16.
Specific design targets will be provided at project kickoff.
PHASE I: Investigate the feasibility and cost effectiveness of various alternate manufacturing processes and material combinations capable of surviving the gun-launch environment while significantly reducing the weight of the identified components.
Define and execute a modeling and simulation test plan that will optimize component designs and material selections, and inform on the decision to switch to new manufacturing processes as well as the associated business case to do so.
Success of Phase I will be the measured by a 50% weight reduction compared to traditional manufacturing methods utilizing the same material.
Submission of a cost analysis is required but will not be used as a measure of success for Phase I.
PHASE II: Based on successful results of Phase I, develop, demonstrate, and fabricate a well-defined solution that is reproducible, and exhibits confidence in transition to both military and commercial markets.
The objective is to conduct further development and optimization of the design and materials that provide the best balance to achieve the requirements, specifications, and metrics listed in this topic.
The Phase II effort will significantly improve upon the performance and efficiency of the conceptual design developed under Phase I.
PHASE III: A full size prototype drawings will be provided by the government for production of prototype component of the best performer whose metrics include weight reduction, strength, and cost from Phase II will be delivered to the Government and integrated into a full-scale demonstration.
A full TDP outlining the manufacturing process as well as material selection will be provided upon completion of Phase III.
Commercial applications include automotive and aircraft engines.
REFERENCES: 1: Umetani and Schmidt 2013 Umetani N.
Ravindra, "Process Evaluation of AISI clearly blackjack chart table apologise Steel Manufactured by Laser Powder Bed Fusion," Journal of Materials Engineering and Performance, vol.
DESCRIPTION: The US Army is in need of an on-board munition sensor package suite that provides the measurement capabilities of a three-axis gyroscope, a three-axis accelerometer, and a three-axis magnetometer.
This innovative solution should have a footprint of 20mm x 20mm.
The sensor package suite must be capable of surviving a minimum of 20,000 Gs.
If the proposed solution relies on an external battery, the sensor package must operate on 3.
A solution with a 20-year shelf life, EMI resistance, and compatibility with military operating and storage conditions is desired.
PHASE I: The contractor shall investigate the feasibility of development of the sensor package and provide a trade-off analysis for the desired measurement capabilities, form factor, cost, and shelf life.
The trade-off analysis must include alternate sensor specifications as well as any possible additions to the package for operational improvements.
A preliminary sensor package design must be completed by the conclusion of phase I.
PHASE II: The contractor shall provide the final design of two possible sensor packages based upon the outcome of Phase I along with input from US government.
The final designs components that can be readily manufactured.
After final designs have been agreed upon, one prototype of the fully assembled board for each design will be delivered for testing at a US government lab.
Manufacturing partners should be engaged early in the phase II process to ensure manufacturability and to shorten the timeline for fielding.
PHASE III: Four fully assembled boards will be provided to USG for final testing and verification.
The final product will be based upon input from initial test results provided by USG to contractor from Phase II.
The contractor will update the board layout and form factor based upon results from Phase II and government requirements for size.
A final TDP package must also be delivered to the government as closeout of this phase.
REFERENCES: 1: Electronic Components for High-g Hardened Packaging 2: Morris S.
Berman 3: Haleh Ardebili, Michael Pecht, Encapsulation Technologies for ElectronicApplications 4: William Andrew, 2009 ISBN 0815519702 "What is Conformal Coating?
These lenses can either be compound, Gradient Index GRINFreeform, or other.
The intent is use such an array in a light field optical configuration to yield a very thin, light camera package that is both fast and compact in size and weight.
DESCRIPTION: The necessity for snipers, soldiers, and crew served weapons operators to rapidly and accurately detect targets on the battlefield is a capability that is of high interest to the department of defense, across all agencies.
It is our desire to create a compact camera system that has a wide field of view as well as high resolution.
Commercially we can find an exemplar in the Lytro approach.
Eurographics Symposium on Rendering, 2006.
Any given micro-lens will have a very short focal length.
We can make the focal length small robust if we form the lenses directly on the CMOS imager as suggested by Thiele et al.
The clustered effective aperture need not be circular, but may be configured in such a way as to nest on a platform, such as a rifle.
In such a case the aperture could wrap around the barrel, thus yielding not only a compact package, but one that would allow for passive ranging and three dimensional image reconstruction as well.
PHASE I: Identify materials, methods and models integrated lens arrays that are compatible with CMOS imagers.
Model the optical systems to ensure that the lenslet arrays will yield suitable image quality for later image reconstruction.
PHASE II: Create an array on a CMOS imager.
This imager should be functional and allow one to read out each of the sub-images.
Transfer the readout into a computer and demonstrate that light field reconstruction is viable.
Contractor shall clearly state in the proposal and final report how the phenomenology provides the unique capability for achieving the design goals.
PHASE III: Optimize the physical properties for military applications.
Prototype a rifle mounted fire control sight using this technology that demonstrates the benefits in performance over currently fielded systems.
Replace conventional electro-optics with the design in a sight that represents the optical performance of a fielded military small arms sighting system.
Create a partnership with industry to commercialize the technology and improve the manufacturability.
Eurographics Symposium on Rendering, 2006.
DESCRIPTION: During the past decade two different technological areas have advanced significantly, i.
In particular, deep convolutional neural networks CNN have demonstrated their potential for accurate object detection and classification.
Such a system would greatly reduce the time and cost required to bring soldier specific image based solutions to the battlefield.
This should include identifying and assessing with costs all critical components necessary to develop the proposed system.
Analysis source include optical design modeling and optimization in which both radiometric and polarimetric response characteristics are predicted, e.
PHASE II: Based on the design criteria established during the Phase I, the candidate will procure all necessary components in order to assemble, test, and demonstrate a fully functional prototype device.
Initial prototype development and testing will include both laboratory and field-based assessment in which standard image quality metrics will be determined, e.
Prototype testing and evaluation will be conducted at a government facility in which optimum functionality will be determined based on range, atmospheric conditions, and tactical scenario.
To be conducted concurrent with the prototype development, the contractor will begin identifying all possible commercialization opportunities and partnerships necessary to successfully bring their developed intellectual property IP to market.
Final report will include system design, experimentation findings, and commercialization plan.
Phase III may include further modification and ruggedization depending on customer needs.
Such evaluation will take place at an appropriate U.
This will also include further maturation of the system in which reduction in size, weight and power SWaP will be examined.
The candidate is expected to pursue civilian applications and additional commercialization opportunities, e.
Pezzaniti, "Remote detection of buried land-mines and IEDs using LWIR polarimetric imaging", Optics Express, Vol.
Felton, "Detection of obscured targets with IR polarimetric imaging", Proc.
SPIE 9072, Detection and Sensing of Mines, Explosive Objects, and Obscured Targets XIX, 90721D, May 29, 2014.
Videen, "Three-dimensional 3D facial recognition using passive LWIR polarimetric imaging", Appl.
Chan, "Improving cross-modal face recognition using polarimetric imaging", Optics Letters vol.
Girshick, "Fast r-cnn", IEEE International Conference on Computer Vision ICCVDecember 7-13 2015Santiago, Chile.
Gurton, "Exploiting polarization-state information for cross-spectrum face recognition", 2015 IEEE 7th International Conference on Biometrics Theory, Applications and Systems BTASSeptember 8-11, 2015Arlington, VA.
Sun, "Spatial pyramid pooling in deep convolutional neural networks for visual recognition", IEEE Trans.
On Pattern Analysis and Machine Intelligence, 37 9pp.
Shaw, "Review of passive imaging polarimetry for remote sensing applications", Appl.
Reale, "MWIR-to-Visible and LWIR-to-Visible Face Recognition Using Pa1rtial Least Squares and Dictionary Learning", Face Recognition Across the Electromagnetic Spectrum, Editor, T.
Bourlai, Springer Press 2015.
KEYWORDS: Artificial Intelligence AIMachine Learning MLThermal Imaging, Polarimetric Imaging, Anomaly Detection, Long-wave Infrared LWIRMid-wave Infrared MidIR TECHNOLOGY AREA S : Electronics OBJECTIVE: Develop an advanced acoustic particle velocity-pressure sensory system that is compact, ruggedized, and modular for anticipated missions involving acoustic localization, signal intelligence and other uses.
Army is seeking research and development in acoustic particle velocity and acoustic pressure sensing technologies that can be implemented for use in acoustic signal detection, localization, tracking, and characterization.
The technologies must be highly modular and capable of integration into atmospheric acoustic detection systems both current and future.
Technologies focusing on modular design are highly desired.
An go here self-aware system is envisioned.
Current microphone array systems are used to detect, localize, and classify acoustic sources.
Dependent upon the source and range of interest, these systems have large foot prints, ranging from several to tens of square meters.
The Army seeks reduced Size, Weight, and Power SWaP systems.
Systems that not only reduce the array system footprint, but also reduce power are highly desired.
Versatility of usage is important, as sources of interest may be harmonic or impulsive, transient or continuous.
Systems may be deployed in a variety of outdoor environments, to include, urban, desert, mountainous, and littoral.
Ruggedized systems that can withstand environmental extremes are a necessity for outdoor emplacement.
Systems may be land-based or airborne, on the move or stationary.
The company will demonstrate the feasibility of the concept in meeting Army needs and will establish that the concept can be developed into a useful product.
Material testing and analytical modeling will establish feasibility.
The concept development effort should assess the importance of several acoustic sensing factors for the APV-P, such as dynamic range, wind noise mitigation, signal fidelity, preservation of waveform, sampling rates, well-defined calibration, and ease of calibration.
Evidence of design optimization of these parameters, as well as a comparison between model predictions and measured performance are required.
Environmental parameters to be measured include wind velocity speed and directionhumidity, temperature, and atmospheric pressure.
Plans for implementing the APV-P will be included as an output of Phase I, along with estimated performance.
The APV-P will be designed to operate at frequencies between 0.
The minimum dynamic range of the APV-P should be -10 dB to 150 dB, though a larger range, on both sides, is desired.
Methods to manage different sound levels should be considered, such as adjustable gains.
Data acquisition should have a minimum sampling rate of 25 kHz, with a minimum of 24-bit resolution.
Sensitivity of the particle velocity detection should be established to correspond with the sensitivity of the pressure sensing.
Of particular concern is calibration of the system; methods for in-field, self-calibration are desired.
A ruggedized system is required, being able to operate in severe environments, including rain and fine-particulate environments.
Environmental parameter sampling should provide for atmospheric thermal-mechanical turbulence characterization at the acoustic scales.
The prototype will be evaluated to determine the capability in meeting performance goals and Army requirements.
System performance will be demonstrated through prototype evaluation and modeling or analytical methods over the required range of parameters.
Evaluation results will be used to refine the prototype into a design that will meet Army requirements.
The APV-P system should include wind noise mitigation.
Documentation should include analyses comparing system response to scientific grade microphones, performance for harmonic and impulsive sources, direction finding compared to conventional systems including azimuth, elevation, and ranging sensitivityhttps://chicago-lawyer.info/blackjack/treasure-chest-casino-blackjack-minimum.html of wind noise mitigation, and preservation of acoustic waveform.
PHASE III: The company will support the Army in transitioning the technology for Army field use.
A compact design is envisioned, allowing emplacement on ground and air vehicles.
The commercial market is typically quick to adopt technology that enhances performance while controlling cost and reducing SWaP.
The company is expected to pursue civilian applications and additional commercialization opportunities.
REFERENCES: 1: L Solomon, L Sim, and J Wind, "Analysis of MEMS-based Acoustic Particle Velocity Sensor for Transient Localization," U.
Army Research Laboratory Technical Report, ARL-TR-5686 2011.
Editors: A Le Pichon, E Blanc, A Hauchercorne 6: Springer International Publishing, 2018.
KEYWORDS: Acoustic Pressure, Acoustic Particle Velocity, Microphone, Acoustic Vector Sensor, Self-aware Sensor TECHNOLOGY AREA S : Electronics OBJECTIVE: Provide algorithms capable of compiling information from multiple frames acquired from a moving unmanned aerial vehicle.
This algorithm will consolidate video data from an unnamed air vehicle in the form of data vectors that represent ground locations from multiple angles of observation.
Army RDECOM CERDEC Night Vision and Electronic Sensors Directorate is supporting protection of combat vehicles through detection of obstacles that threaten maneuverability in battlespace environments.
We are developing sensors mounted on unmanned air vehicles to detect and localize landmines, natural or manmade topography, and surface obstacles that limit maneuverability or threaten the continue reading vehicle.
To aid in this goal we will collect data over an environment from multiple look angles to improve our knowledge of the objects or conditions at ground locations.
We believe that having multiple samples at a ground location will produce better features for subsequent algorithms.
We seek assistance in this area from qualified companies who can implement algorithms that will identify terrain features from multiple video frames collected by an airborne imaging system.
Algorithms should process this data to determine 3D point clouds and subsequently assign to these points data associated with that location from multiple cameras and look angles.
Topography and surface objects in the scene should be accounted for in the algorithms to appropriately register data to particular ground locations.
The means of achieving this objective may include, but are not blackjack chips value to, structure from motion, image transforms and photogrammetry.
It is desirable that 3D information about the environment be obtained as an intermediate product.
A potential benefit of this level of processing is the ability for the algorithm to discriminate above ground clutter from surface level terrain or obstacles.
Likewise, information about the relative attitude of the air platform would be beneficial.
Contractor data may be used to develop the algorithms, but as these algorithms mature Government provided data will be utilized to assess performance on data collected at Government test sites.
This algorithm will preferentially operate using image data alone.
Inertial Measurement Unit IMUGlobal Position System GPSand height data may be brought to bear if significant improvements blackjack camo stencils output quality are achievable; however preference is given to methods that operate pokerist mac GPS denied environments.
Subsequent detection processing of the assembled feature vectors should be considered in the context of improving resolution and registration accuracy, but this solicitation is does not encompass advanced automatic target detection development.
PHASE I: This effort should identify algorithms capable of registering commit leather blackjacks and saps think data to ground locations.
Preliminary testing of contractor or modeled data should be performed to determine the ground sampling density achievable as a function of standoff distance, magnification and pixel size.
The impact of optical distortions, frame rate, range of collection and nadir vs.
The final report will be include the expected performance as a function of system parameters and sufficient information to determine the necessary conditions for sensors and platforms to achieve accurate image registration to ground locations.
PHASE II: This effort will implement the algorithm as software to produce 3D point clouds and associated image intensity data from Government data.
Data assessment methods will be developed to determine the accuracy and stability of algorithm for various controlled data collections as well as field conditions without fiducial targets.
The algorithm will show a path to continuous operation at realistic frame rates.
The algorithm will be implementable on processing hardware scaled for size, weight, and power appropriate for an unmanned aerial vehicle.
The algorithm should be demonstrated on such a processor or demonstrated to specify the processing and computation needs required.
Resolution is desired on the order of 10cm for select regions of interest.
Thus, the holistic algorithm may require trivial pre-screener processing to limit processing regions requiring improved resolution.
The Phase II final report will include detailed system software and hardware design, system capability and limitations, detailed summary of testing and results, lessons learned, critical technology and performance risks.
PHASE III: The Phase III goal is to develop and implement accurate image registration algorithms on processors for UAVs.
This may be combined as a complete product for commercial sales, or as an algorithmic add on that utilizes Government or commercial sensors and platforms.
This phase will improve accuracy of the methods and produce consistent feature vectors of image data associated with locations in the scene.
REFERENCES: 1: Irschara, Arnold, Christopher Zach, Jan-Michael Frahm, and Horst Bischof.
IEEE Conference on, pp.
DESCRIPTION: Applications of Deep Learning and Machine Learning to imagery and video have been dramatic in the last decade.
However, these achievements have been almost entirely based on visible band imagery and video.
The data requirements of these algorithms are enormous, and developers have been able to rely on masses of readily available visible band data.
Militarily significant IR data does not currently exist in the quantities and varieties necessary to fully leverage the advantages of Deep Learning.
What is needed a set of techniques and algorithms which can artificially generate militarily significant as in specific localities and target types IR video and imagery in entirety and to augment existing IR data with novel prescribed objects and targets.
Success and promise has recently been shown by Generative Adversarial Networks.
However, these image constructions are mostly intended for visual effect.
Much higher fidelity is essential to training AiTRs.
Also artificial IR modeling systems exist at Night Vision and Electronic Sensors Directorate NVESD.
This effort aims at overcoming data limitations listed above and enhancing realism of current NVESD modeling systems.
The goal is to support an IR AiTR effective fieldable system—enhancing vehicle threat detection and avoidance.
This effort directly supports Army Modernization Priority: Next Generation Combat Vehicle NGCV —benefitting the automation associated with the NGCV through improved algorithm performance.
This effort will enable NGCV sensors to rapidly determine external threats and alleviate operator fatigue via automation of surveillance and navigational functions.
PHASE I: Show proof of concept for Deep Generative Modeling algorithms for IR imagery and video synthesis.
Show proof of concept for algorithms to greatly improve realism of synthetic imagery.
Integrate algorithms into comprehensive algorithm suite.
Test algorithms against existing NVESD modeling methodologies.
Demonstrate feasibility of techniques in creating IR video sequences.
Distribute demonstration code to Government for independent verification.
Successful testing at the end of Phase 1 must show a level of algorithmic achievement such that potential Phase 2 development demands few fundamental breakthroughs but would be a natural continuation and development of Phase 1 activity.
PHASE II: Complete primary algorithmic development.
Complete implementation of algorithms.
Test completed algorithms on government controlled data.
System must achieve 25% improvement in classification rate and false alarm rate over AiTR algorithms trained on real imagery alone using government baseline AiTR algorithm.
Principle deliverables are the algorithms.
paroli betting system blackjack algorithms will be fully deliverable to government in order to demonstrate and further test system capability.
Successful testing at end of Phase 2 must show level of algorithmic achievement such that potential Phase 3 algorithmic development demands no major breakthroughs but would be a natural continuation and development of Phase 2 activity.
PHASE III: Complete final algorithmic development.
Complete final software system implementation of algorithms.
Test completed algorithms on government controlled data.
System must achieve 25% improvement in classification rate and false alarm rate over algorithms trained on real imagery alone using government baseline AiTR algorithm.
Documented algorithms along with system software will be fully deliverable to government in order to demonstrate and further test system capability.
Applications of the system will be in NVESD Multi-Function Display Program, vehicle navigation packages, and AiTR systems.
Civilian applications remarkable, blackjack stand on soft 17 opinion be in night surveillance, crowd monitoring, navigation aids, and devices requiring rapid adaptation your 7bitcasino final new environments.
REFERENCES: 1: Steven A.
Goldstein 3: Jeffrey S.
Klein 4: James Talamonti 5: Franklin Tanner 6: Shane Zabel 7: Philip A.
Sallee 8: Lisa McCoy, "Generative Adversarial Networks for Classification", 2017 IEEE Applied Imagery Pattern Recognition Workshop AIPR.
Channappayya, "Improving the Visual Quality of Generative Adversarial Network GAN -Generated Images Using the Multi-Scale Structural Similarity Index ", 2018 25th IEEE International Conference on Image Processing ICIP.
KEYWORDS: Deep Learning, Generative Adversarial Networks, Aided Target Recognition, Neural Networks, Infrared Video TECHNOLOGY AREA S : Electronics OBJECTIVE: Evaluate, develop and demonstrate the novel application of emerging commercial technologies for heterogeneous integration of infrared photodetector arrays and CMOS-based multiplexing circuitry.
DESCRIPTION: The Army needs the highest performance infrared sensors for tactical and strategic overmatch.
Mission-specific applications for high-sensitivity sensors extend across multiple infrared bands, including long wavelength 8-12 microns.
These requirements have led to the development of infrared focal plane arrays IRFPA with large formats ~ megapixel and small pixel pitch ~ 10 micron.
Such IRFPAs consist of an array of photodetectors hybridized to a CMOS-based multiplexing circuit ROICwhich reads out the photo-generated current to create useful imagery and information.
ROIC design has evolved to improve sensor performance and to include more on-chip functionality, such as digitization and signal processing.
Such 3D integration offers potential, significant cost savings for IRFPA fabrication, particularly, if wafer-to-wafer integration can be realized.
PHASE I: The performer shall evaluate and analyze 3D integration technology in the context of IRFPA fabrication: i.
This analysis shall include technical, cost and security considerations.
This analysis shall consist of a trade study of various processes and parameters constrained by compatibility with IRFPA processing and operation: for example, comparison of wafer-to-wafer, die-to-wafer and die-to-die integration modes.
Based upon the results of this analysis, the performer shall develop a plan to develop, to implement and to demonstrate 3D integration technology in an IRFPA product article source is relevant to Army requirements.
PHASE II: The performer shall design and develop a 3D integration process that is compatible with a relevant IRFPA product based upon analysis and planning of Phase I.
The performer shall implement, demonstrate, test and evaluate the resulting process, in hardware, in a relevant IRFPA product.
Dual use applications include: machine vision, autonomous vehicles, security, process control, environmental monitoring, scientific instruments, and astronomy.
REFERENCES: 1: Wang, L, et al.
DESCRIPTION: High resolution microdisplays are essential for providing the human interface to high resolution digital sensors and wide field of view augmented and mixed reality vision systems used for Soldier Lethality.
Reduction of power, bandwidth, and head borne heat of these microdisplays is important for all DoD application, but it is especially important for untethered infantry.
A 2,048 x 2,048 reconfigurable microdisplay capable of reduced power operation with a moveable full-resolution window within a field of reduced resolution has been developed under government contract and is available as GFE for this effort, but an alternative display solution is also acceptable.
Coupling a reconfigurable display with an eyepiece and an eye tracker would allow power to be saved by keeping the high resolution area of the display only where the fovea is located.
This project would determine if a foveated display can provide sufficient performance compared to a 100% full resolution display while reducing power and bandwidth.
PHASE I: Create a notional design for the demonstrator.
Build a demonstrator that can be large scale desktop display and computer that shows eye tracking and reduces the resolution electronically or optically of the display in areas outside the fovea TRL 4.
The demonstrator will be used to examine the visual performance for detecting and responding to peripheral visual cues based on the interaction of the foveal area profile vs.
The demonstrator will include a way to measure the power for full vs.
PHASE III: Implement the foveated display design into a military HMD, possibly partnering with a HMD manufacturer TRL 6.
Address integration issues, cost, and power reduction vs.
REFERENCES: 1: Clarence E.
Army Aeromedical Research Laboratory 2009 2: Kyle R.
Attenuator will capable of changing from high optical transmission for an unobscured view of the environment to low transmission to enhance the contrast of the display versus the ambient.
DESCRIPTION: See-through displays, which are used for situational awareness and targeting for Soldier Lethality and Future Vertical Lift, can be overwhelmed by high level ambient light such that the content of the display is not readable.
A contrast of 1.
Reducing the transmission of the see-through optic, such as a visor, can aid with display contrast and readability, but the transmission needs to be high in some operations, especially at night, to allow the user to see details in the real environment through the optic.
Arbitrarily driving the brightness of the display source brighter would enable readability, but it may increase power and thermal management demands beyond allowable limits, especially for untethered infantry.
It also limits the display and optical technologies available for augmented reality solutions.
See-through displays are also subject to external hazards and threats that occluded systems are not.
A continuously variable attenuator can allow full daylight readability in bright ambient conditions, a clear view of the real world in night operations, and can have built in protections against hazards and threats.
One potential form of the variable attenuator will be to provide the ability to transition bi-directionally between a broad-band, visually neutral, low transmission state of not more than 20% and a broadband, optically neutral, high transmission state of at least 80% in under 1 second.
An automatic read article of the transmission is optional, but a manual adjustment override is essential.
Hazard and threat protection is also optional.
Address spectrum, level of attenuation, switching speeds, localized attenuation, and potential hazard and threat protection.
Provide sample demonstrators of attenuator technology TRL 4.
Phase I demonstrators may utilize planar substrates.
Develop a fully functional demonstrator that is integrated with a see-through head worn display TRL 6.
PHASE III: Integrate with a military AR HMD, possibly partnering with an HMD manufacturer for this effort TRL 7.
Apply technology to larger HUDs in aircraft and to vehicle windows.
Implement hazard and threat protection if not already included.
REFERENCES: 1: Clarence E.
Army Aeromedical Research Laboratory 2009 2: Russell S.
Rash, "Daylight luminance requirements for full-color, see-through helmet-mounted display systems", SPIE Optical Engineering Vol.
Examples of these advances include colloidal semiconductor quantum dots, quantum wire carbon nanotubes, and graphene with combined structures that could potentially enable highly beneficial detector designs for photoconductors, photodiodes, or field effect transistors 1-3.
These and similar technologies may be the future steps for high-speed, compact, lightweight, and low-cost sensor operation.
In this topic, high-speed, high-performance infrared detector concepts operating at room temperature are being pursued to support small, lightweight, low-power soldier sensor systems that perform better than current imagers.
Detectors should operate at very high speeds like quantum detectors, and at room-temperature like bolometers.
For the future Army dismounted soldiers, low cost and small size, weight and power SWaP infrared sensors are critical to equip our soldiers in the battlefield.
This topic has significant impact on the CFTs Soldier Lethality, as well as Future Vertical Lift and Next Gen Combat Vehicles.
The detailed detector performance includes but is not limited to 1 High speed at 120Hz operation, 2 High performance comparable to or better than the current bolometers at room temperature, 3 Suitability for large format, small pitch focal plane array fabrication, 4 Compatibility with existing readout integrated circuitry for detector integration, and 5 Cost lower than current bolometers.
The cutoff wavelength can be in the long- or mid-wavelength infrared spectrum.
It is highly desired to bodog free blackjack the capability to capture a thermal image without light.
Low-light-level, visible or near infrared detectors will also be considered.
A suitable digital readout integrated circuit ROIC should be identified for uncooled detector use.
PHASE I: In Phase I, an innovative detector concept should be modeled and designed and detectors should be grown and processed to demonstrate single element diodes.
PHASE III: Develop and execute a plan to market and manufacture the new focal plane arrays FPAs.
Assist Army in transitioning this technology to the appropriate Prime Contractor s for the engineering integration and testing.
REFERENCES: 1: "MWIR Imaging With Low Cost Colloidal Quantum Dot Films", Christopher Buurmaa, Richard E.
Ciania, Jered S Feldmana, Christoph H.
Greina, and Philippe Guyot-Sionnestb, Proc.
Keo, Linda Hoglund, Robert Rosenberg, Robert Kowalczyk, Arezou Khoshakhlagh, Anita Fisher, David Z.
Ting, and Sarath D.
Gunapala, Applied Physics Letters 105, 023512 2014.
KEYWORDS: Uncooled Infrared Detectors, Focal Plane Arrays, Quantum Detectors × A point-of-care assay to determine soldier dengue exposure and enable rapid, mass, cost-efficient dengue vaccination programs of military personnel TECHNOLOGY AREA S : Bio Medical OBJECTIVE: Develop a specific cost-effective point-of-care assay to rapidly identify dengue exposure history in the warfighter enabling force protection readiness and high-throughput mass dengue vaccination programs DESCRIPTION: Dengue virus DENV is a growing threat to tropical regions and the warfighter.
The four dengue virus serotypes complicate risk management and readiness.
The current, approved, gold-standard to accurately determine dengue exposure history is to use plaque-reduction neutralizing assays PRNT.
The turn-around time for a PRNT result is too long when large-scale dengue vaccine programs are underway, particularly for time-sensitive mass deployments.
Waiting for PRNT results would be unfeasible even for routine recruit basic training vaccination programs.
This assay was designed primarily as a clinical ZIKV diagnostic assay.
This would be vital for time-sensitive dengue vaccination programs of large volumes of troops before deployment when it would not be possible to obtain their serostatus in a feasible time frame.
It would also remove the need to perform thousands to millions of expensive, time-demanding PRNT assays in existing Department of Defense laboratories which currently do not have the capacity to perform such a large volume of reference dengue diagnostic tests.
A point of care dengue specific exposure device will reduce risk of any current or future dengue vaccine and pre-deployment dengue exposure testing will identify soldiers and general population that are at increased risk of severe disease when traveling or deploying to high risk dengue regions of the world.
Of note this device would not be an acute disease diagnostic to identify pathogens causing fever and dengue disease.
While current acute point-of-care febrile disease diagnostic platforms can estimate primary versus secondary dengue infection, they are calibrated and validated to do so only during an acute febrile illness and they cannot accurately detect prior dengue exposure in the asymptomatic host which would typically have far lower circulating levels of anti-flavivirus antibodies.
PHASE I: By the end of Phase I the successful applicant will have: i Conceptualized the assay to include potential targets of dengue verse other related flavivirus specificity and demonstrate with design and data package supporting claims of specificity.
This validation will include metrics of assay validity and reliability, with estimates of uncertainty around these metrics.
This validation must address the broad genetic and antigenic diversity of DENV by global location.
The expected performance parameters would be a sensitivity greater than 90% and a specificity greater than 90%, although the target performance characteristics may depend on the setting of use see Phase III and the pre-test probability of disease exposure and can be coordinated and refined with the COR.
PHASE III: The expected Phase III end-state is an FDA approved, low-cost, point-of-care, closed-system, easy-to-use and easy-to-interpret assay which can be used on a relatively low volume of easily accessible biospecimen.
The transfer from research to operational capacity would occur via the biotechnological industry pathway, such that appropriate scale up and feasible unit costs can be accommodated.
It is envisaged that this point-of-care test that could be operated by a nurse or other healthcare professional in the office without the need for laboratory expertise.
A similar consumer group may be civilians presenting to a travel clinic for pre-travel dengue risk advice and vaccination.
This end-product would also be critical for civilian population dengue vaccination programs and we would envisage it would be used on a population scale in dengue endemic regions to facilitate widespread dengue vaccination programs which are projected to greatly reduce the overall burden of dengue in many tropical regions, but which are currently restricted by host serostatus safety concerns.
REFERENCES: 1: Balmaseda A, Stettler K, Medialdea-Carrera R, Collado D et al.
Antibody-based assay discriminates Zika virus infection from other flaviviruses.
Proc Natl Acad Sci U S A.
Epub 2017 Jul 17.
Dengue and US military operations from the Spanish-American War through today.
Human antibody responses after dengue virus infection are highly cross-reactive to Zika virus.
Proc Natl Acad Sci USA.
Effect of Dengue Serostatus on Dengue Vaccine Safety and Efficacy.
N Engl J Med.
Clinical development and regulatory points for consideration for second-generation live attenuated dengue vaccines.
DESCRIPTION: The Army requires advancement in Autonomous Target Recognition ATR algorithms for seekers in gun launched applications.
Currently, seekers are capable of target detection in low clutter environments.
To field a fully effective weapon that is also safe for use in conditions where there is high fratricide or collateral damage concern, the ability to discriminate between target types and between friend and foe rapidly within minutes and under extremely dynamic conditions is required.
The algorithms shall be capable of operating on emerging commercial GPU products suitable to 155mm artillery SWaP-C constraints.
Detailed requirements will be provided after contract award.
PHASE I: Phase I will consist of development of prototype algorithms on representative hardware demonstrated in laboratory simulated environments.
A final report will document testing results and present the top level plan to continue development in Phase II.
The result of Phase II will be a prototype design, including applicable technical data, which will be integrated into current and future munition designs for advanced target recognition.
PHASE III: Upon success of Phase II, these technologies would be transitioned to munitions currently in development.
REFERENCES: 1: CONVOLUTIONAL NEURAL NETWORKS AS FEATURE EXTRACTORS FOR DATA-SCARCEVISUALSEARCHES, Hichem ben Abdallah, September 2016.
DESCRIPTION: The Army relies on radiography inspection e.
Interpreting the visual results of the inspections is a challenge and requires highly trained individuals Level III Radiographers to determine what, if any, problems actually exist.
As this technology is meant to be incorporated in a production line, the expectation is that it will support three dimensional inspection and interpretation of defects at a production rate of up to 1 unit per minute, and items up to 6.
Defects include cavities, porosity, piping, voids, gaps, low density, annular rings, cracks and inclusions ranging from 0.
The technology must reside on a standard computer system linked online free practice blackjack the inspection equipment and receive the electronic images from the radiography system.
Specific interface requirements will be provided after contract award.
This topic will also develop and deliver the output screens that provide the proper data and information that a Level II radiographer is trained to understand.
PHASE I: Phase I will consist of development of prototype algorithms on representative hardware to be defined prior to contract award demonstrated in laboratory simulated environments.
The government may also provide actual images obtained during prior government testing.
A final report will document testing results and present the top level plan to continue development in Phase II.
The result of Phase II will be a prototype design, including applicable technical data, which will be integrated into current and future radiography inspection systems at multiple government locations.
REFERENCES: 1: "Automated Defect Recognition and Identification in Digital Radiography", P.
Arteta, 2017 IEEE Winter Conference on Applications of Computer Vision WACVSanta Rosa, CA, 2017, pp.
Signal-Image Technology and Internet-Based Systems SITIS2014 Tenth International Conference on.
The SCA decouples waveform software from its platform-specific software and hardware, facilitates waveform software re-use, and minimizes development expenditures.
The main objective is to develop an automated testing platform as a dynamic testing method for the SCA 4.
This effort develops an extensible environment for the construction, organization, execution, and summary of automated, reproducible compliance tests on SCA 4.
DESCRIPTION: The desired solution will provide an automated test platform for Tactical Communications Waveforms and Applications against the SCA v4.
The resultant product of this effort would be transitioned to the Joint Tactical Network Center.
The tool employs both dynamic and static testing approaches since some of the SCA requirements may not be verified by dynamic testing.
Phase II will provide an automated compliance test solution for SCA 4.
The tool employs both dynamic and static testing approaches since some of the SCA requirements may not be verified by dynamic testing.
PHASE III: Phase III will integrate the tool developed in Phase II with the SCAv4.
The STS tool verify tactical radios against the SCA v4.
The reports will include all technical challenges, technical risk, and progress against the schedule.
REFERENCES: 1: Joint Tactical Network Center, Software Communications Architecture Specification, Version 4.
V 6 March 2018SCA v4.
DESCRIPTION: The 28-V Lithium-ion 6T drop-in replacement battery Li-ion 6T is a critical technology to enhance energy storage to improve warfighting performance across the Army, Marines, and Navy.
The Li-ion 6T is a drop-in replacement for legacy Lead-Acid 6T batteries for starting, lighting, and ignition SLI and silent-watch applications, and provides the same form, fit, and expanded function, including increased silent watch time, significantly extended cycle life, and faster recharge time.
Deficiencies in Li-ion 6T manufacturing inspection technologies and processes could result in three possible undesirable outcomes: 1 battery products with latent defects, in either the cells or BMS, which causes premature failure or safety issues in the field such as an internal cell short ; 2 battery products with deficient performance for their intended function as a result of poorly matched cells such as poor cycle life ; or 3 low yield resulting in increased production cost through waste.
Technologies developed should be specifically for Li-ion battery pack production processes versus cell production processes and should be specifically focused on cell selection at the start of the pack production process and end-of-line testing of the final product at the end of the pack production process.
Currently, cells within the Li-ion 6T battery are matched in many cases simply by capacity and internal resistance and manufacturing cell selection equipment and processes are not designed specifically with Li-ion 6T in mind.
Cell selection solutions should take into account technologies such as internal resistance measurement, internal short detection, electro-impedance spectroscopy, calorimetry, and neural networks as well as other innovative analysis techniques.
End-of-line test solutions must be able to account for the whole operational voltage and temperature range of the battery as well as be capable of simulating pulse events such as cold crank.
The systems and solutions developed should be open-architecture to the greatest extent possible.
Technology developed should be generally applicable and adaptable to all Li-ion 6T products as well as to all low-voltage commercial Li-ion battery packs.
Innovative solutions developed for pack end-of-line testing shall include the ability to determine compliance to all MIL-PRF-32565 periodic production inspection Practice blackjack tournament tests and have a secure way of reporting results of PPI testing to the Qualifying Activity such as public-private key encryption.
PHASE I: Identify and determine the engineering, technology, and hardware and software needed to develop this concept.
End-of-line test technologies developed shall include all listed PPI testing in Table VII of the MIL-PRF-32565, including: Physical characteristics, Dimensions and weights, Terminal posts and threaded sockets, Full charge capacity, Cranking amps, Charging, Charge acceptance, Safety protections, Workmanship, and Defects.
Solutions developed shall improve yield and reduce waste, and consequently improve production costs, by at least 5%.
Automated PPI testing using technologies link under this effort shall reduce the time required for completion of PPI by half.
Drawings showing realistic designs based on engineering studies are expected deliverables.
A bill of materials and volume part costs for the Phase I designs should also be developed.
This phase also needs to address the blackjack game what is a identified in the above description.
PHASE Blackjack minimums vegas Develop and integrate prototype hardware and software into high-volume manufacturing equipment using the designs and technologies developed in Phase I.
Testing of the Phase II design shall include mock manufacturing runs using small production batches of Li-ion 6T cells and Click at this page 6T batteries.
A bill of materials and volume part costs for the Phase II design should also be developed.
PHASE III: This phase will begin installation and integration of the solutions developed in Phase II into military Li-ion 6T and commercial Li-ion pack production processes and blackjack camo stencils low- to high-volume manufacturing lines.
REFERENCES: 1: Lambert, Simon M.
DESCRIPTION: Recent advances in the computing world has allowed for algorithmic advances in the detection and characterization of the electromagnetic spectrum EMS.
Specifically, the incorporation of such things as neural networks and training processes has elevated artificial intelligence AI and machine learning ML as key innovation areas for detecting, characterizing and cataloging highly complex signal types in the EMS.
The unit would be able to detect and characterization various signal types and modulations.
It would also provide performance and monitoring tools to provide real-time feedback to operators.
The incorporation of data analytics for validation and visualization would be included in the unit.
The system would follow a Modular, Open Systems Approach MOSA to allow integration into a variety of Army systems.
The MOSA approach would also provide extensible ML and Deep Learning DL functions to expand upon key features and signal types.
The system would contain only Commercial, Off-The-Shelf COTS products.
PHASE I: Develop system design that includes artificial intelligence AI and machine learning ML algorithms and concepts, hardware and software specifications, and protocol operation both internal and external.
PHASE II: Develop and demonstrate a prototype system in a realistic environment.
Conduct testing to prove feasibility over extended operating conditions.
Demonstrate that the product can be integrated and utilized in a tactical system with minor modifications to include form, fit, function changes and minor interface upgrades.
Demonstration will provide key decision points on interoperability, MOSA integration, and tactical feasibility.
REFERENCES: 1: Szepesvari, Caleb.
Algorithms for Reinforcement Learning.
Batch Normalization: Accelerating Deep Network Training by Reducing Internal Covariate Shift.
Implementation of machine learning applications on a fixed-point DSP.
DESCRIPTION: While Aerostat systems are an essential tool for support to ongoing combat operations their utility is limited during high intensity conflicts due to their static nature, inability to rapidly redeploy within theater and inability to provide persistent Intelligence, Surveillance and Reconnaissance ISR in support of Wide Area Operations.
Despite these shortfalls Aerostats are in high demand from our coalition partners.
It is anticipated that the airship functionality could potentially be obtained thru normal P3I efforts and little to no additional program costs.
Our fires community can provide strategic fires hundreds of miles further than our current sensors can currently provide persistent coverage.
UAV and space based assets are vulnerable to enemy targeting and are too expensive to provide persistent low cost wide area coverage.
Once targeted UAV and space based sensors are difficult and expensive to reconstitute in any reasonable period of time.
Follow on efforts would further scale this capability for use in tactical, operational and strategic missions.
Effort would enable Aerostats to operate autonomously or as remote controlled unmanned Airships that can be statically deployed via tethers as they are now but with the ability to drop its tether and self-deploy within its theater while conducting limited wide area operations LCP ISR.
Endurance for static operations would be 30 days continuous operations and 7 days during airship mode operations with an operational range of 2000 miles.
While these systems would be vulnerable to enemy targeting and destruction, the systems would be considered attritable and due to their low cost; easily replaceable.
It is anticipated that enemy action would be counterproductive due to the necessary enemy disclosure that would result.
PHASE I: Carry out a feasibility study for leveraging current commercial Airship designs for military use and demonstrate potential capabilities via use of commercial products as military prototypes.
Phase I will define factors for a Phase II sensor demonstration for Fires, Cyber, and Force Protection.
PHASE II: Demonstrate capabilities using the commercial prototype for Fires, Cyber and Force Protection.
PHASE III: Develop prototype aka battle type that would be deployed into a combat theater for proof of concept assessment.
Deeson, An Illustrated History of Airships Bourne End, Bucks: Spurbooks Limited, 197315-20.
Largess, "Reviving the Naval Airship," NAVAL FORCES vol XI, No 1 1990 : 13.
KEYWORDS: Aerostat, LCPISR, Unmanned-airship TECHNOLOGY AREA S : Electronics OBJECTIVE: The Army has interest in sensors with passive and low probability of intercept acquisition and weapon cueing capabilities applicable to air defense in support of Short Range Air Defense SHORAD system missions.
Small innovative business insights to support highly survivable short to moderate range Army Air and Missile Defense AMD acquisition and fire control sensors initiatives is sought.
DESCRIPTION: State-of-the-Art or emerging passive or low probability of intercept sensor technologies are needed as complementary components of the SHORAD integrated sensor suite to support SHORAD unit real time Situational Awareness SAtarget acquisition and weapon cueing.
On-board passive and low probability of intercept sensors must be compatible with supported unit battlefield environments and vehicle form factors.
The prioritized targets to be addressed are: 1.
Nano- to Class III Unmanned Air System UASto include individual, multiple and swarm presentations.
Rocket, Artillery and Mortar RAM to include precision indirect fires and salvo attacks.
Sensors are required to perform target acquisition at all mission phases and to support target engagement on the move or on a short halt.
Preference is for the sensor to support high volume of fire required to a large number of different target types in a combined saturation attack.
Sensors are required to perform target acquisition at all mission phases and to support target engagement on the move or on a short halt.
Preference is for the sensor to support high volume of fire required to a large number of different target types in a combined saturation attack.
Sensor related elements of the kill chain include: 1.
Fusion with other SHORAD sensors.
Positive identification, Identification of Friend or Foe or classification of non-combatant.
Weapon cueing with possible fire control capability and kill assessment of kinetic and non-kinetic engagements.
PHASE I: Investigate and research technologies that can be incorporated into SHORAD systems, and are complementary to existing SHORAD sensors, to build and field sensor systems that are extremely difficult to detect, or attack, and are able to provide actionable information to the Soldier concerning active threats.
Some technologies may be commercial-off-the-shelf tools that can be innovatively employed to operationally harden systems operate with minimal signature in the battlefield ground mobile environment.
Some technologies may be new and, as yet, not well known.
False targets must be minimized, but sensors must provide actionable data in real time.
Sensors could be signature based, behavior based or may leverage a technique that is yet to be developed.
Investigations should include estimated development and production costs to support preliminary government budgeting activities.
Once investigation and research of potential technology is complete, the offeror will, in an unclassified format, identify implementation options in a Phase 1 report.
PHASE II: Using the technology and approach es identified in Phase I, and adding classified Phase II technologies if needed, develop, fabricate and validate a prototype sensor.
The sensor should fully address integration, size-weight-and-power SWAPand any system performance or impacts.
Given a viable technical approach and performance, estimate and refine development, support and production costs to be included with technical concept data and delivered prototype implementation.
PHASE III: Transition the Phase II product into a fieldable sensor prototype for detailed technical and operational testing.
Educational Notes RTO-EN-SET-086, Paper 4.
DESCRIPTION: Improved armor protection is a fundamental component of lethality, one of the six army modernization priorities of the Army.
Current ballistic protection of the HGU-56P helmet is limited to a.
Multiple ballistic material technologies have been published in the last year suggesting ballistic improvement to the aviation helmet can be achieved with minimal weight increase.
Objective is to provide US National Institute of Justice NIJ Level II 9mm ballistic protection.
Current helmet shell protection is called out in 1680-ALSE-101, Aircrew Integrated Helmet System Fabrication Specification.
PHASE I: This effort shall create a study identifying the most promising ballistic improvement technologies allowing retrofit of the aviator helmet with the lowest weight and cost to enable production.
The study shall also project durability and retrofit time for each solution.
A demonstration of ballistic performance of the technology proposed is required.
Options for introduction of the new material s proposed include retrofit of the existing helmet most desirablereplacement of the helmet shell, replacement of the helmet liner foam, or replacement of both the liner and foam lease desirable.
Ballistic improvement can be projected as a function of keeping total helmet weight equal or less than existing helmet of each size.
A threshold requirement of 10% ballistic improvement to the existing helmet is required as an entry criteria for Phase II.
PHASE II: The best two solutions identified in phase I will be used to build or retrofit a helmet and tested to quantify ballistic improvement.
Four helmet s will be furnished to the vendor for retrofit and ballistic testing.
The retrofit process for the helmet will be documented for each solution.
A summary report at the end of the study shall document ballistic performance improvement of each solution, identify exact weight impact to the helmet, identify retrofit time and cost of each solution and assess durability of each solution.
The contractor shall update the product specification with the new ballistic performance capability to reflect the improved armor protection and a projection of increased weight based on prototype production.
Perform bench testing for all helmet specification requirements on production representative prototypes.
Deliverables will include test plan, test report, updated helmet specification reflecting measured improvement in ballistic performance, minutes for all meetings conducted with the vendor, presentation slides for retrofit application of ballistic material, a white paper detailing the retrofit process of the ballistic material, and a cost report detailing retrofit cost as a function of helmet quantity from a minimum of 50 and up to 1000 at a time.
PHASE III: Develop production processes for best retrofit solution found in Phase II.
Update the helmet item specification to reflect final production process weight.
Aviation helmets used throughout DOD may find retrofit application for this same process.
Commercial jet engines may find an ultra light coating application capable of resisting turbine blade failure causing injury or death to a passenger aircraft.
This topic addresses lighter tactical power generation that increases the ability to operate semi-independently; a critical enabling technology to the Soldier Lethality Army Modernization Priority.
The Power Generation for Individual Soldier device shall provide a minimum of 6 watts of continuous uninterrupted power for 24 hours.
The device, including fuel source as applicable, shall have a volume not to exceed 50 cubic inches and shall not weigh more than 2.
No dimension shall exceed 12 inches.
It shall operate during day and night.
PHASE I: Develop click here system design and provide a performance specification as part of the Final Technical Report.
Include unit cost projections in the Technical Report.
A breadboard demonstration of proposed design is encouraged.
PHASE II: Design, fabricate and demonstrate a prototype system in an operational relevant environment.
Deliver two TRL 6 prototypes to the Government.
Deliver Final Technical Report, which includes a product specification and estimated unit production cost.
PHASE III: A wearable power generation system has multiple uses in military and civilian operations.
Besides the obvious first responders' and outdoors' types please click for source applications, this device could potentially end the current problem with handheld and other power consuming devices, where their batteries run out of power before consumers have a chance to find a place to plug in.
With the constant growth of wireless services and the capabilities of wearable devices, current battery technology is not keeping up with power consumption.
This could be the solution.
Phase III shall consist of the development of the producibility of this item for military use.
REFERENCES: 1: Stirling engine, from Wikipedia, the free encyclopedia 2: Renewable energy, from Wikipedia, the free encyclopedia 3: Photovoltaics, from Wikipedia, the free encyclopedia 4: Biofuel, from Wikipedia, the free encyclopedia 5: Photosynthesis, from Wikipedia, the free encyclopedia 6: Micropower, from Wikipedia, the free encyclopedia KEYWORDS: Wearable, Power, Generation, Continuous, Lightweight, Small TECHNOLOGY AREA S : Weapons OBJECTIVE: To increase overall Soldier Lethality Capability by providing ballistic calculators, weapon fire control devices, and related apps, with immediate, real-time muzzle velocity information after each shot fired to automatically update ballistic computations to enhance accuracy of follow-on shots.
Small arms exterior ballistic calculations, used to predict an aim point in order to hit a target, are based on either estimated muzzle velocities or measured muzzle velocities which are typically taken when zeroing a weapon and before executing a mission.
However, muzzle velocities will typically change over time and during operational-use based on several dynamic factors to include barrel cleanliness and wear; rate-of-fire; variations in ammunition composition; ammunition and bore temperatures; and when available weapon suppressor conditions.
Real-time muzzle velocity measurements, provided in a closed-loop feedback schema, would allow fire control and ballistic calculators to better account for and compensate for these unknown and constantly changing variables, thereby increasing aiming accuracy and probability of target hit on successive shots.
It is envisioned that this measuring device would eventually be affixed to or incorporated within a weapon barrel.
The closed loop feedback between the muzzle velocity measurement device and ballistic solver s would be accomplished via either hard-wired or wireless communications.
This effort would ultimately increase mission effectiveness and overall soldier lethality.
PHASE I: Research and propose a viable cost-effective technical solution that satisfies the stated objective.
In order to expedite an initial proof of concept, PMSW would like to focus on applying this desired capability to current medium-to-long range sniper weapons since 1 sniper teams require the utmost in aiming accuracy and 2 they currently rely on muzzle velocities with ballistic solvers in determining scope reticle offset holds for target engagements.
Potential applicable sniper weapon platforms for consideration include the 7.
It is envisioned that once proven, the technology could be scaled to other mission area weapons as fire control capabilities proliferate, especially with Next Generation Squad Weapons.
As such and to facilitate Phase I efforts, a surrogate sniper weapon, optic, and ammunition, comparable to the M110, should be used.
This accuracy is commensurate with the Government tested accuracy of the Magnetospeed Ballistic Chronograph Part : MS V3BTwhich was also online blackjack watch celebrity by the Army, as its Small Arms Ballistic Chronograph SABCand added to the ASAK in FY 2015.
All work performed in Phase I shall be provided in a final report that identifies the best conceptual solution.
Breadboard tests to demonstrate technical feasibility are encouraged.
PHASE II: Design, develop, build, and deliver six 6 prototype Real-time Muzzle Velocity Feedback Systems based on Phase I recommendations that can be demonstrated with a weapon platform that is comparable to the M110 SASS.
The M110 SASS is a source variant of the commercially available 7.
The RMVFS is intended to integrate with a ballistic solver software to effectively use that muzzle velocity data to calculate real-time exterior ballistics and provide any adjusted aim-points.
The system needs to be tested to prove that the RMVFS muzzle velocities meet the objective accuracy requirements and that muzzle velocity data can be passed and used in real-time by a ballistic solver.
Phase II culminates with a report that includes test and demonstration results.
A detailed proposal will be developed that delineates required efforts to have a TRL-7 system available to be demonstrated in a military environment as a potential Phase III follow-on effort.
The system has potential commercial applicability for law check this out, hunters, and target shooters.
DESCRIPTION: FeMnAl is a lightweight, high-strength steel alloy with Fe-28Mn-9.
The Army is interested in using this steel to reduce weight in a variety of ground vehicle platforms.
While a high-alloy steel, it is a single phase, with age-hardenability.
This means there are fewer concerns with rapid solidification, as martensite cannot form, and heat treatment can be used to control the hardness of the final part.
Similarly, there is growth in the development of additive manufacturing repair techniques for ground vehicles.
However, there is not currently a similar high-alloy steel powder available.
Additive repairs requires compatibility with this high alloy steel, which in turn requires unique powder compositions.
The unique chemistry of this alloy is expected to be challenging, and require innovative processes to manufacturing in powder form.
This steel has been produced via traditional metal manufacturing techniques, in both cast and wrought forms.
No attempt has been made to develop a powder form of this material.
PHASE I: In Phase I, the small business will assess the capability to make high alloy powders near this composition.
This powder will be compatible with Directed Energy Deposition, with a powder size of 60 to 125µm.
Compositional please click for source will be required.
High rating will be placed on compositional evaluation using wet chemistry methods, due to known limitations of optical emission and spark spectroscopy for this composition.
Feasibility of process will be demonstrated by production of a small batch of powder of the intended composition.
Deliverables shall include materials data and physical powder samples.
PHASE II: In Phase II, the small business will improve processing to make powder within compositional tolerances, targeting uniformity throughout the batch.
The final powder should easily transition to customers interested in light weighting, particularly in wear-sensitive regions.
Powder would be made available to Programs of Record, such as PdM Abrams, for purchase and use for repair of their systems in which FeMnAl has been integrated.
It may also be used in future design of specific components with significant weight restrictions.
REFERENCES: 1: Zimmerman, B, Allen, E.
System to power robotic vehicles, ground vehicle auxiliary systems or exoskeletons.
System durability will be increased as well.
In addition, SOFC systems also have high power densities 1high electrical efficiencies 1a lower acoustic signature than internal combustion engines 2produce water as a byproduct 3have the highest tolerance for sulfur in the fuel of any fuel cell type 3 and do not require the use of precious metal catalysts for operation 3.
These advantages make SOFC systems i.
Smaller scale SOFC systems currently exist that would fit into a similar space claim as proposed here, but the power supplied by those systems is lower than 2kW.
The 2kW of power generated by the SOFC stack, with the system capable of up to 13kW intermittent power spikes using internal batteries, proposed in this topic is viewed as an adequate starting power for use with robotic vehicles, auxiliary systems on ground vehicles and exoskeleton systems.
Advancement of new novel materials used within the system construction such as catalysts used in electrode construction and oxygen transport materials used in electrolyte constructionincreased catalyst loading, optimized system design and innovative geometries used in stack design to increase active surface area can all be investigated and developed to address this issue.
The SOFC system i.
SOFC stack, internal batteries for 13kW power, fuel and balance of you basic strategy chart blackjack apprentice tempting components will have the following requirements in addition to meeting the 2kW power.
The system will produce 36-48V of electricity and be able to supply power using the attached fuel source for 4-5 hours continuously.
The system will be able to thermally cycle between 50-100 times without the SOFC system power degrading below 2kW excluding internal battery power.
The system will be able to operate for at least 1,000 hours combined operation time or single continuous use without the SOFC system power degrading below 2kW excluding internal battery power.
The system will have a start time of 30 minutes or less to achieve 2kW of continuous power with 13kW intermittent power.
The system will be capable of being operated with compressed hydrogen gas or with light hydrocarbon fuels such as butane, propane or methane.
These system requirements are standard with less compact SOFC systems, which should be preserved for this opinion, metodo hi lo blackjack opinion compact system as well 45.
PHASE I: This phase will focus on conducting a feasibility study to determine the best approach to achieve the SOFC systems requirements listed above.
This study will be used to identify materials and different fabrication approaches that will allow the SOFC system to achieve the desired system landing saganing blackjack eagles casino output.
The feasibility study will also focus on methods of increasing system durability and methods of eliminating failure points during operation.
PHASE II: Phase II will focus on optimizing the SOFC system design and conducting durability experiments.
Experiments will be conducted in stages first by using single cells or short stacks 5-cell stacks.
Stack size will then gradually be increased and each new stack size will be tested to identify degradation and durability failure modes until a full stack passes testing criteria.
SOFC system power will be increased to 2kW by conducting experiments on the system to identify points of parasitic losses and novel approaches of manufacturing the SOFC system to minimize those losses through different material choices or system design.
A preliminary investigation should also be completed in order to determine the cost of fabricating the SOFC devices and stacks.
PHASE III: The system should be scalable to provide power to the military in such areas as: 1.
Robots and exoskeletons used for reconnaissance and bomb disposal, 2.
Drone aircraft used for reconnaissance and short to medium ranged strikes, and 3.
Auxiliary power to ground vehicles to save energy costs and for silent watch capability.
The system should also be scalable for the commercial market to provide power in areas of: 1.
Power generation for homes, 2.
Auxiliary power for ground commercial vehicles, and 3.
Auxiliary power for light commercial aircraft.
The system should also conform to particular dimensions of a space claim and provide the required amount of power for each application.
An additional objective of this topic is to grow the industrial base of the US Air Force.
This topic will reach companies that can complete a feasibility study and prototype validated concepts in accelerated Phase I and II schedules.
This topic is specifically aimed at later stage development rather than earlier stage basic science and research.
DESCRIPTION: The Air Force is a large and complex organizations that consists of many functions that have similar counterparts in the commercial sector.
We are interested in exploring innovative technology domains that have demonstrated clear commercial value in the non-defense sector i.
We recognize that it is impossible to cover every technological area with the SBIR topics, thus this topic is intended to be a call for open ideas and technologies that cover topics that may not be currently listed i.
It is important that any potential solutions have a high probability of keeping pace with the technological change and thus should be closely tied to commercial technologies and solutions that will help support the development of the solution.
Solutions for this topic should be focused on the three areas listed below and should try to meet as many of these as possible.
Technical feasibility — There should be minimal technical risk to the overall solution.
The best solutions will have demonstrated technical feasibility by source the solution being used broadly by other customers, especially in the non-defense space.
If the solution has not demonstrated technical feasibility in the non-defense space, the offeror s may provide alternative evidence to indicate technical feasibility such as initial lab tests, use of the product with defense customers and other forms of evidence.
Financial Sustainability — The offeror s should demonstrate financial sustainability of the solution and the offeror s.
The best solutions will demonstrate this by sales of the solution to non-defense clients and other sources of private investment.
If the solution has not demonstrated financial sustainability by non-defense sales or private investment, the offeror s may provide other evidence of financial sustainability such as other governmental aid, sales to defense customers, and other forms of evidence that help explain the financial sustainability.
Defense Need — The offeror s should demonstrate that they have an understanding of the fit between their solution and defense stakeholders.
In summary - proposals for this topic should demonstrate a high probability to quickly find product-market fit between an Air Force end user and the proposed solution through adaptation of a non-defense commercial solution.
This can be done through a proposal with a mature non-defense technical solution and a starting point to find an Air Force customer.
BROAD FOCUS AREAS AND SPECIFIC USER NEEDS FOR 19.
Thus, if your solution can help address one of these Focus Areas, there is likely to be a good number of Air Force End-Users and customers that you can interact with in your phase I feasibility study and an increased likelihood for matching funding.
Note that this does not change link requirement to demonstrate the defense need as listed above, but may complement it.
PHASE I: Validate the product-market fit between the proposed solution and a potential USAF stakeholder and define a clear and immediately actionable plan for running a trial with the proposed solution and the proposed AF customer.
This feasibility study should directly address: 1.
Clearly identify who the prime potential AF end user s and AF transition customer the user and customer will likely be two different people and articulate how they would use your solution s i.
Deeply explore the problem or benefit area s which are to be addressed by the solution s - specifically focusing on how this solution will impact the end user of the solution.
Define clear objectives and measurable key results for a potential trail of the proposed solution with the identified Air Force end user s.
Clearly identify any additional specific stakeholders beyond the end user s who will be critical to the success of any potential trial.
This includes, but is not limited to, program offices, contracting offices, finance offices, information security offices and environmental protection offices.
Describe how the solution differs from the non-defense commercial offering to solve the Air Force need - i.
Describe the cost and feasibility of integration with current mission-specific products.
Describe if and how the demonstration can be used by other DoD or governmental customers The funds obligated on the resulting Phase I SBIR contracts are to be used for the sole purpose of conducting a thorough feasibility study using scientific experiments, laboratory studies, commercial research and interviews.
Prototypes may be developed with SBIR funds during Phase I studies to better address the risks and potential payoffs in innovative technologies.
PHASE II: Develop, install, integrate and demonstrate a prototype system determined to be the most feasible solution during the Phase I feasibility study.
This demonstration should focus specifically on: 1.
Evaluating the proposed solution against the objectives and measurable key results as defined in the phase I feasibility study.
Describing in detail how the solution differs from the non-defense commercial offering to solve the Air Force need and how it can be scaled to be adopted widely i.
A clear transition path for the proposed solution that takes into account input from all affected stakeholders including but not limited to: end users, engineering, sustainment, contracting, finance, legal, and cyber security.
Specific details about how the solution can integrate with other current and potential future solutions.
How the solution can be sustainable i.
Clearly identify other specific DoD or governmental customers who want to use the solution.
PHASE III: PHASE III DUAL USE APPLICATIONS: This is the main goal of this topic, we intend for many of the solutions to go straight from Phase I to Phase III as soon as the product-market fit has been verified.
The contractor will transition the adapted non-defense commercial solution to provide expanded mission capability to a broad range of potential government and civilian users and alternate mission applications.
Due to the large amount of expected interest in this topic, we will not be answering individual questions through e-mail, except in rare cases.
Instead we will be holding a teleconference to address all questions in an efficient manner.
This topic will be updated with the final call-in details as soon as the date is finalized.
This SBIR is NOT awarding grants, and is awarding contracts, when registering in SAM.
If you are only registered to compete for grants, you will be ineligible for this topic.
We are working to move fast, please register in SAMs and if already registered please double check your CAGE codes, company name, address information, DUNS numbers, ect.
In order to ensure this, please include, in your 15-slide deck, a screenshot from SAM.
It is the responsibility of the contractor to ensure that the data in the proposal and the data in SAM.
In order to keep pace with the fast timeline, if the purchase orders are not signed and returned to the contracting office within 5 business days of receipt, a Phase I award will not be issued.
If a company submits multiple technically acceptable proposals, only the proposal with the highest evaluation will be awarded.
If multiple proposals are evaluated to be equal, the government will decide which proposal to award based upon the needs of the Air Force.
All awards are subject to the availability of funds and contracting negotiations.
While these are firm fixed price contracts, it is important for the companies to include the cost volume in the SBIR online application with reasonable fidelity in order to determine the reasonableness of the proposed effort.
Foreign National is defined in 22 CFR 120.
§ 1101 a 20nor a protected individual 8 U.
§ 1324b a 3.
Additional information may be required during negotiations to verify eligibility.
Even if eligible, participation may be restricted due to U.
Future Foundry: A New Strategic Approach to Military-Technical Advantage.
The Mission Model Canvas — An Adapted Business Model Canvas for Mission-Driven Organizations.
US Department of Defense.
This topic will reach companies that can complete a feasibility study and prototype validated concepts in accelerated Phase I and II schedules.
This topic is specifically aimed at later stage development check this out than earlier stage basic science and research.
DESCRIPTION: The Air Force Program Executive Office for Digital is responsible for the acquisition of software and weapons systems including development and fielding worldwide aerospace command and control applications.
The Air Force wishes to stay at the cutting edge of these technologies and seeks click at this page partner with innovative small businesses continue reading blackjack camo stencils have solutions to Air Force challenges.
These are the high level challenge areas for which the Air Force is interested in novel solutions: 1.
Security Tools and Services: Tools to monitor the security of unclassified software development environments, to include security of on premise and cloud-hosted applications, as well as technologies that enhance the security of software development systems, pipelines, and code repositories.
Edge as a Service: Technologies to operate and maintain continuous and secure cloud-native operation in low-bandwidth environments.
Enterprise Platform Tools: Technologies for enterprise platform design, development, and delivery, as well as technologies that facilitate application and infrastructure monitoring, API management and integration, legacy system virtualization and hosting, and container orchestrations and security.
PHASE I: "Validate the product-market fit between the proposed solution and a potential USAF stakeholder and define a clear and immediately actionable plan for running a trial with the proposed solution and the proposed AF customer.
This feasibility study should directly address: 1.
Clearly identify who the prime potential AF end user s is and articulate how they would use your solution s i.
Deeply explore the problem or benefit area s which are to be addressed by the solution s - specifically focusing on how this solution will impact the end user of the solution.
Define clear objectives and measurable key results for a potential trail of the proposed solution with the identified Air Force end user s.
Clearly identify any additional specific stakeholders beyond the end user s who will be critical to the success of any potential trial.
This includes, but is not limited to, program offices, contracting offices, finance offices, information security offices and environmental protection offices.
Describe the cost and feasibility of integration with current mission-specific products.
Describe if and how the demonstration can be used by other DoD or governmental customers.
Describe technology related development that is required to successfully field the solution.
The funds obligated on the resulting Phase I SBIR contracts are to be used for the sole purpose of conducting a thorough feasibility study using scientific experiments, laboratory studies, commercial research and interviews.
Prototypes may be developed with SBIR funds during Phase I studies to better address the risks and potential payoffs in innovative technologies.
This demonstration should focus specifically on: 1.
Evaluating the proposed solution against the objectives and measurable key results as defined in the phase I feasibility study.
Describing in detail how the solution can be scaled to be adopted widely i.
A clear transition path for the proposed solution that takes into account input from all affected stakeholders including but not limited to: end users, engineering, sustainment, contracting, finance, legal, and cyber security.
Specific details about how the solution can integrate with other current and potential future solutions.
How the solution can be sustainable i.
Clearly identify other specific DoD or governmental customers who want to use the solution PHASE III: "The Primary goal of SBIR is Phase III.
The contractor will pursue commercialization of the various technologies developed in Phase II for transitioning expanded mission capability to a broad range of potential government and civilian users and alternate mission applications.
Due to the large amount of expected interest in this topic, we will not be answering individual questions through e-mail, except in rare cases.
Instead we will be holding a teleconference to address all questions in an efficient manner.
This topic will be updated with the final call-in details as soon as the date is finalized.
This SBIR is not awarding grants, but contracts, when registering in SAM.
If you are only registered to compete for grants, you will be ineligible for this topic.
We are working to move fast, please register in SAMs and if already registered please double check your CAGE codes, company name, address information, DUNS numbers, ect.
If they are not correct at time of submission, you will be ineligible for this topic.
In order to ensure this, please include, in your 15-slide deck, a screenshot from SAM.
Companies must be present at the Kessel Run Pitch event July 2019 at the Kessel Run Software Factory located at 1 Beacon Street, Boston, MA and complete their pitch to AF evaluators in order to receive an award.
REFERENCES: 1: "A Revolution in Acquisition and Product Support.
This topic will reach companies that can complete a feasibility study and prototype validated concepts in accelerated Phase I and II schedules.
This topic is specifically aimed at later stage development rather than earlier stage basic science and research.
DESCRIPTION: This effort is a partnership between the Air Force Program Executive Office for Digital PEO Digitalthe Air Force Research Lab AFRLand the Tri-Service C-sUAS Swarm group.
The Air Force PEO Digital is responsible for the acquisition of software and weapons systems including support for UAS air traffic avionics and control software, UAS applications to environmental sensing, and development of innovative C-sUAS technologies for defense of critical facilities.
The AFRL leads the discovery, development and delivery of warfighting technologies for air, space and cyberspace forces including swarm autonomy and decision making, as well as open system approaches for UAS and subsystems like communications, human interfaces, and sensorsetc.
The Air Force wishes to stay at the cutting edge of these technologies and seeks to partner with innovative small businesses that may have solutions to Air Force challenges.
These are the high level challenge areas for which the Air Force is interested in novel solutions: 1.
UAS payloads to defeat other UAS 2.
UAS just click for source optical, infrared, acoustic, radar, etc identification software 3.
UAS avionics open software trust and verification technologies 4.
UAS sensing for weather hazard avoidance 5.
UAS sensing for characterization of environmental conditions wind, hydrology, RF spectrum, etc 6.
UAS applications to resilient PNT mitigation of GPS degradation, etc 8.
Small UAS design assurance and airworthiness certification 9.
Counter Swarm technologies 10.
Agile technology insertion for UAS 11.
PHASE I: "Validate the product-market fit between the proposed solution and a potential USAF stakeholder and define a clear and immediately actionable plan for running a trial with the proposed solution and the proposed AF customer.
This feasibility study should directly address: 1.
Clearly identify who the prime potential AF end user s is and articulate how they would use your solution s i.
Deeply explore the problem or benefit area s which are to be addressed by the solution s - specifically focusing on how this solution will impact the end user of the solution.
Define clear objectives and measurable key results for a potential trail of the proposed solution with the identified Air Force end user s.
Clearly identify any additional specific stakeholders beyond the end user s who will be critical to the success of any potential trial.
This includes, but is not limited to, program offices, contracting offices, finance offices, information security offices and environmental protection offices.
Describe the cost and feasibility of integration with current mission-specific products.
Describe if and how the demonstration can be used by other DoD or governmental customers.
Describe technology related development that is required to successfully field the solution.
The funds obligated on the resulting Phase I SBIR contracts are to be used for the sole purpose of conducting a thorough feasibility study using scientific experiments, laboratory studies, commercial research and interviews.
Prototypes may be developed with SBIR funds during Phase I studies to better address the risks and potential payoffs in innovative technologies.
This demonstration should focus specifically on: 1.
Evaluating the proposed solution against the objectives and measurable key results as defined $1 blackjack the phase I feasibility study.
Describing in detail how the solution can be scaled to be adopted widely i.
A clear transition path for the proposed solution that takes into account input from all affected stakeholders including but not limited to: end users, engineering, sustainment, contracting, finance, legal, and cyber security.
Specific details about how the solution can integrate with other current and potential future solutions.
How the solution can be sustainable i.
Clearly identify other specific DoD or governmental customers who want to use the solution" PHASE III: "The Primary goal of SBIR is Phase III.
The contractor will pursue commercialization of the various technologies developed in Phase II for transitioning expanded mission capability to a broad range of potential government and civilian users and alternate mission applications.
Due to the large amount of expected interest in this topic, we will not be answering individual questions through e-mail, except in rare cases.
Instead we will be holding a teleconference to address all questions in an efficient manner.
This topic will be updated with the final call-in details as soon as the date is finalized.
This SBIR is not awarding grants, but contracts, when registering in SAM.
If you are only registered to compete for grants, you will be ineligible for this topic.
We are working to move fast, please register in SAMs and if already registered please double check your CAGE codes, company name, address information, DUNS numbers, ect.
If they are not correct at time of submission, you will be ineligible for this topic.
In order to ensure this, please include, in your 15-slide deck, a screenshot from SAM.
REFERENCES: 1: "A Revolution in Acquisition and Product Support.
Air Force, Small Unmanned Aircraft Systems SUAS Flight Plan: 2016-2036, 30 Apr 2016.
The fuel pyrolytic and oxidation intermediate species measured are those involved in key combustion reaction pathways for AF and other DOD propulsion systems, and their measurement enables characterization of fuel combustion chemistry and supports combustion model development efforts.
Primary Arms Digital camo stencil How to Paint tutorial
Western Camo Personalized Valentine. Delight your child and their friends with PRE-Personalized Valentines › Non folding cards measure 4.75" x 3.5"
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