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SBC: Firefly Technologies Topic: T3
Firefly, in collaboration with Rochester Institute of Technology, proposes an STTR program for the development of a wide-bandgap GaP-based space solar cell capable of efficient operation at temperatures above 300oC. Efficiency enhancement will be achieved by the introduction of InGaP quantum wells within the active region of the wide-gap base material. The introduction of these nanoscale features ...STTR Phase I 2010 National Aeronautics and Space Administration
SBC: SRICO INC Topic: A12aT023
SRICO proposes to combine metamaterial narrowband absorbers and SRICO-proprietary thin film lithium tantalate (TFLT) pyroelectric thermal detectors to produce ultra low cost, size, weight and power (SWaP) room temperature stand-off chemical sensors. Metamaterial narrowband absorber elements will be integrated into the TFLT pyroelectric detector process to provide conversion of radiation to heat, w ...STTR Phase I 2013 Department of DefenseArmy
SBC: UES INC Topic: AF09BT30
Military applications for CBRNE/GWTO and C4ISR require R&D for materials to protect personnel and equipment. However, challenges remain in experimental synthesis and characterization of new materials, such as providing insight into observed properties for further advancement. Thus, it is essential to develop a predictive modeling and simulation approach that will not only provide a fundamental u ...STTR Phase I 2010 Department of DefenseAir Force
SBC: BFE Acquisition Sub II, LLC Topic: A10AT004
Thermopile arrays manufactured using integrated process compatible materials and micro-machining will provide high performance with low manufacturing cost. Black Forest Engineering (BFE) teamed with Case Western Reserve University will design thermopiles using silicon based semiconductors and compare performance. Low cost thermopiles, differentially coupled with advanced BFE CMOS readout, will pr ...STTR Phase I 2010 Department of DefenseArmy
SBC: Silicon Informatics, Inc. Topic: A10AT012
Highly scalable parallel random number generators (RNGs) will be developed, evaluated and implemented for use in high performance computing on thousands of multi-core processors and general purpose graphics processing units. The main contributions are: (a) design and implementation of new parallel test methods that capture the inter-stream correlations exhibited in practice and complement the curr ...STTR Phase I 2010 Department of DefenseArmy
SBC: TTC TECHNOLOGIES, INC. Topic: AF09BT10
A computational and experimental research program is proposed to develop and validate a high-fidelity 3D non-equilibrium magnetohydrodynamic (MHD) plasma compressible flow code for advanced aerospace applications. The code will incorporate a physics-based kinetic model of air plasma with non-equilibrium conductivity sustained by an externally applied electric field. The model will include electron ...STTR Phase I 2010 Department of DefenseAir Force
SBC: UES INC Topic: 10a
Currently the commercially available technologies for H2 separation such as pressure swing adsorption and cryogenic distillation are very energy intensive. Membrane technologies can be very energy efficient; but for high selective membranes low flux and high cost are the major challenges that frustrate commercialization. Recently, cermet has shown promise because of less precious metal usage and m ...STTR Phase I 2010 Department of Energy
SBC: MAINSTREAM ENGINEERING CORP Topic: OSD09T002
Military shelters currently use electrically driven Environmental Control Units (ECUs) to provide cooling for the air inside the shelter. The ECU is vapor compression cycle powered by a diesel generator, operating on JP-8 fuel. Other than fueling jet engines, the largest drain on U.S. military fuel supplies in current operations comes from running generators at forward operating bases. In hot cli ...STTR Phase I 2010 Department of DefenseNavy
SBC: CORNERSTONE RESEARCH GROUP INC Topic: ST13A006
Federal Aviation Administration Advisory Circular 20-107B provides guidance on the achievement of compliance with Title 14 of the Code of Federal Regulations regarding airworthiness type certification requirements for composite aircraft structures necessiSTTR Phase I 2013 Department of DefenseDefense Advanced Research Projects Agency
SBC: Florida Turbine Technologies Inc. Topic: ST13A005
Pressure gain combustion has the potential to significantly improve the specific fuel consumption for gas turbine engines by realizing a pressure rise through the combustor as opposed to a pressure drop. One drawback to this form of combustion is the cyclSTTR Phase I 2013 Department of DefenseDefense Advanced Research Projects Agency