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SBC: STREAMLINE NUMERICS INC Topic: T901
The innovation proposed here is a high performance, high fidelity simulation capability to enable accurate, fast and robust simulation of unsteady turbulent, reacting flows involving cryogenic propellants (such as LOX/LH2 and LOX/LCH4). The key features of this proposed capability are: (a) Hybrid RANS-LES (HRLES) methodology, and (b) flamelet modeling for turbulent combustion incorporated in a pr ...STTR Phase I 2010 National Aeronautics and Space Administration
SBC: T3 SCIENTIFIC LLC Topic: 10c
Providing a reliable, clean and economical energy source is a priority of the US government. The challenge is to use coal, a secured and economical energy source, to produce clean hydrogen fuel to support domestic and global green economy with near-zero emission. Conventional separation technology and even developmental technology do not satisfy all of the requirements for hydrogen production from ...STTR Phase I 2010 Department of Energy
SBC: TECHNOLOGY ASSESSMENT AND TRANSFER, INC. Topic: 26a
The conversion of carbon-containing feedstocks to hydrogen and syngas will play important roles in the 21st century in the form of large plants for converting natural gas to liquids, hydrocarbons to chemicals, biomass to fuels and chemicals, and small units for powering fuel cells. Advancements in hydrogen membrane separation technologies have the potential to reduce costs, improve efficiency, and ...STTR Phase I 2010 Department of Energy
SBC: TECHNO-SCIENCES, LLC Topic: AF09BT39
Conversion of sunlight to chemical fuels by artificial photosynthesis has been a long-sought goal. The major goal of the proposed effort is to develop a novel fuel-generating (e.g., hydrogen) photolytic device, which consists of a semiconductor nanowire decorated with metal nanoparticles. The project targets a low-cost technology by fabricating and utilizing the nanowire-nanoparticle conjugate de ...STTR Phase I 2010 Department of DefenseAir Force
SBC: TECH-X CORPORATION Topic: AF09BT10
We propose to develop a commercial weakly ionized plasma modeling capability based off of Tech-X’s high energy density plasma fluid code TxFluids. The new additions will be able to be used to model hypersonic vehicle physics including shock waves, plasma chemistry and innovative techniques for blackout mitigation and hypersonic vehicle control through the application of electric and/or magnetic ...STTR Phase I 2010 Department of DefenseAir Force
SBC: TECH-X CORPORATION Topic: T301
Computational tools that accurately predict the performance of electric propulsion devices are highly desirable by NASA and the broader electric propulsion community. Large investments in running the long duration test programs (> 20 kHrs) at NASA GRC can be reduced with computer models and allow more focus on exploring the NEXT ion thruster design for future space missions. The current state of e ...STTR Phase I 2010 National Aeronautics and Space Administration
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: N10AT028
Thermo-mechanical processes of turbine disks have been progressively improved to meet microstructural requirements tailored for advanced, sustainable high temperature performances. However, the chemistry of typical Ni-base turbine disk alloys is very complex, and yields a variety of phases and microstructural anomalies under different thermo-mechanical heat treatments. These microstructural hetero ...STTR Phase I 2010 Department of DefenseNavy
SBC: UES INC Topic: MDA09T002
This Phase I STTR program seeks a new fabrication method to produce stronger (>100 kpsi) and tougher (>10 MPa m1/2) ultra high temperature Ta-Hf-C-based composites (UHTC) with an outstanding oxidation resistance for use as thermal protection systems for hypersonic applications, as well as for advanced rocket nozzle throat components. UES will apply a novel "Top Down" approach to control the micro ...STTR Phase I 2010 Department of DefenseMissile Defense Agency
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