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Remtech Inc.
UEI: N/A
# of Employees: N/A
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: No
Award Charts
Award Listing
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Hypersonic Thermal Protection Design Tools
Amount: $80,000.00A cost efficient aerothermal design tool is required for redesign for the Holloman rocket sled TPS for operating conditions in excess of Mach 10. Current hardware was designed with peak velocities at ...
SBIRPhase I1995Department of Defense Air Force -
Miniature Independent Data Acquisition Package
Amount: $70,000.00N/A
SBIRPhase I1995National Aeronautics and Space Administration -
Measurements of Gas-Surface Interactions from Plume Constituents on Spacecraft Surfaces
Amount: $50,000.00N/A
SBIRPhase I1993National Aeronautics and Space Administration -
RAREFIED GAS EFFECTS ON AEROBRAKING/REENTRY VEHICLES WITH WAKES
Amount: $467,378.00AEROBRAKING VEHICLES (AOTV, ASTV AND VEHICLES TO MARS) ARE GOING TO MAKE SEVERAL PASSES AND DIP LOW IN THE TRANSITIONAL REGIME IN ORDER TO ACHIEVE THE DESIRED REDUCTION IN VELOCITY. EVEN AT THE LOWEST ...
SBIRPhase II1992National Aeronautics and Space Administration -
SEMI-RIGID, TAILORABLE, COST-OPTIMIZED NLS HEAT SHIELD
Amount: $50,000.00N/A
SBIRPhase I1992National Aeronautics and Space Administration -
SURFACE ROUGHNESS FEATURES FORMULATION FOR AIRCRAFT ICING
Amount: $50,000.00N/A
SBIRPhase I1992National Aeronautics and Space Administration -
AUOTMATED VIBRATION AND THERMAL ANALYSIS OF ELECTRONIC DEVICES
Amount: $53,410.00AN AUTOMATED VIBRATION AND THERMAL ASSESSMENT OF ELECTRONIC DEVICES USING CLOSED FORM PROCEDURES IS PROPOSED. IT WILL ADDRESS MECHANICAL DESIGN THAT IS CONSISTANT WITH SIMPLIFIED ANALYSIS. DESIGNS THA ...
SBIRPhase I1991Department of Defense Air Force -
RAREFIED GAS EFFECTS ON AEROBRAKING/REENTRY VEHICLES WITH WAKES
Amount: $49,408.00N/A
SBIRPhase I1991National Aeronautics and Space Administration -
INTEGRATED CAD VENTING ANALYSIS PACKAGE
Amount: $50,000.00REMTECH, INC. PROPOSES TO DEVELOP A STANDARDIZED COMPUTER CODE TO ANALYZE THE VENTING OF COMPONENTS FOR WHICH PRESSURETRANSIENTS EXIST, RANGING FROM PRESSURIZED TO FREE-MOLECULARVACUUM CONDITIONS. THI ...
SBIRPhase I1990National Aeronautics and Space Administration -
COUPLING OF UNSTEADY FLUID DYNAMICS AND STRUCTURE IN LOW DENSITY HIGH SPEED FLOWS
Amount: $50,000.00AN INNOVATIVE COMPUTATIONAL TECHNIQUE IS REQUIRED TO COUPLE A COMPRESSIBLE TIME-ACCURATE CFD CODE WITH A STRUCTURAL ANALYSIS CODE TO SIMULATE FLUIDS-STRUCTURES INTERACTION. A LITERATURE SURVEY SHOWS T ...
SBIRPhase I1990National Aeronautics and Space Administration