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SBC: SLS, LLC Topic: ST13A003
We propose a gravitational-radiation military communications system which is based on quantum-mechanical parametric amplifiers, oscillators, and transducers. In the transmitter at a remote site A, a parametric amplifier using a Planck-mass-scale, moving sSTTR 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
SBC: HYPERCOMP INC Topic: ST13A005
Pressure gain combustion (PGC) offers means to a more efficient energy use in propulsion and power generation devices. Integrating PGC concepts in gas turbine engines often results in highly unsteady flow conditions at turbine inlet. Further, the backpresSTTR Phase I 2013 Department of DefenseDefense Advanced Research Projects Agency
SBC: AEGIS TECHNOLOGY, INC. Topic: OSD12T06
This proposed project is to develop a novel class of high-temperature, high-energy-product permanent magnets with minimized rare-earth element based on a two-phase (Sm2Fe17N3)1-x(Co35Fe65)x (0STTR Phase I 2013 Department of DefenseAir Force
SBC: APPLIED OPTRONICS CORP Topic: ST13A002
To solve the DARPA need for high-performance MEMS-based optomechanical accelerometers, Applied Optronics proposes to develop a Compact Integrated Silicon Nitride Microresonator Accelerometer (OPTIMA), which is based on a combination of a high-Q silicon niSTTR Phase I 2013 Department of DefenseDefense Advanced Research Projects Agency
SBC: OTHER LAB, INC. Topic: ST13A006
Carbon fiber reinforced polymer composite materials are light and strong, however the development of composite aerostructures has been expensive and slow. Custom tooling is required for each part produced, significant capital investment is required to winSTTR Phase I 2013 Department of DefenseDefense Advanced Research Projects Agency
SBC: HYPERCOMP INC Topic: AF12BT15
ABSTRACT: Stability phenomena that are of vital interest in liquid rocket motor development involve a confluence of diverse physics and interactions across many system components. Any comprehensive, self-consistent numerical model is burdened by a very large computational mesh, stiff unsteady processes which limit permissible time step, and the need to perform tedious, repeated calculations for a ...STTR Phase I 2013 Department of DefenseAir Force
SBC: NEXTGEN AERONAUTICS, INC. Topic: ST13A006
NextGen Aeronautics (NextGen) and University of Southern California (USC, RI) team of experienced composite materials, structural design, and analyses personnel are responding to the opportunity to develop stochastically verified composite structural desiSTTR Phase I 2013 Department of DefenseDefense Advanced Research Projects Agency
SBC: Metacomp Technologies, Inc. Topic: AF12BT15
ABSTRACT: The proposed work aims to build a physics-based rapid turnaround simulation capability for resolving combustion dynamics in liquid rocket engines operating at trans-critical and supercritical flow regimes. The methodology will explore both Reduced-Order Methods and Reduced-Basis Methods as potential candidates for efficient unsteady flow simulation, data storage and retrieval, and data ...STTR Phase I 2013 Department of DefenseAir Force
SBC: New Jersey Microsystems, Inc. Topic: A10aT004
New Jersey Microsystems, Inc proposes to develop an economical thermopile array with sensitivity maximum in the long wave infrared region (LWIR). Current infrared detectors are too expensive to be widely deployed in large numbers. The proposed MEMS technology is simpler, more manufacturable, and therefore less expensive than existing bolometers and ferroelectric devices based on rare earth and ...STTR Phase II 2013 Department of DefenseArmy