HYPERSONICS

Basic Information

164 FERNE COURT
PALO ALTO, CA, 94306 0460

Company Profile

n/a

Additional Details

Field Value
DUNS: 178051900
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 4


  1. Coupling of Computational Fluid Dynamics (CFD), Reentry Vehicle Surface Ablations, and In-Depth Conductions

    Amount: $948,238.00

    The proposed innovation consists of developing and testing an integrated computational tool capable of predicting simultaneously the hypersonic flow over a reentry vehicle and the response of its ther ...

    SBIR Phase II 2006 Air Force Department of Defense
  2. Coupling of Computational Fluid Dynamics (CFD), Reentry Vehicle Surface Ablations, and In-Depth Conductions

    Amount: $98,993.00

    The proposed innovation consists of developing a stand-alone computational tool to predict simultaneously the hypersonic flowfield and the thermal response of the heatshield of vehicles entering the a ...

    SBIR Phase I 2005 Air Force Department of Defense
  3. Unitary Numerical Method For Flow And Heatshield Analysis

    Amount: $69,904.00

    N/A

    SBIR Phase I 1995 National Aeronautics and Space Administration
  4. RF Performance Measurements in Simulated Reentry Environments

    Amount: $72,789.00

    N/A

    SBIR Phase I 1993 Air Force Department of Defense
  5. Development of Base-Flow Computer Code

    Amount: $63,000.00

    N/A

    SBIR Phase I 1993 Air Force Department of Defense
  6. INNOVATIVE MODEL FOR REACTING FLOWS

    Amount: $416,239.00

    THIS PROJECT EXPLORES THE BENEFITS OF A NEW COMPUTATIONAL MODEL FOR REACTING FLOWS. IT APPLIES TO NON-EQUILIBRIUM FLOWS, IN GENERAL, BUT IS SPECIALLY DESIGNED TO ADDRESS THE FREQUENT CONDITION IN HYPE ...

    SBIR Phase II 1992 National Aeronautics and Space Administration
  7. ADVANCED AEROTHERMOCHEMISTRY ALGORITHM

    Amount: $535,000.00

    A COMPUTER BASED ALGORITHM IS PROPOSED THAT INTEGRTES AN ADVANCED NAVIER-STOKES HYPERSONIC FLOW SOLVER WITH STATE-OF-THE-ART MATERIAL RESPONSE COMPUTER CODES TO CREATE A POWERFUL TOOL FOR REENTRY VEHI ...

    SBIR Phase II 1991 Air Force Department of Defense
  8. INNOVATIVE MODEL FOR REACTING FLOWS

    Amount: $48,662.00

    N/A

    SBIR Phase I 1991 National Aeronautics and Space Administration
  9. ADVANCED AEROTHERMOCHEMISTRY ALGORITHM

    Amount: $69,743.00

    N/A

    SBIR Phase I 1990 Air Force Department of Defense
  10. COMPUTATIONAL TOOL FOR ANTENNA WINDOW ABLATION

    Amount: $439,791.00

    CURRENT SHAPE-CHANGE COMPUTER CODES USED TO PREDICT ANTENNA WINDOW (AW) EROSION PLACE EMPHASIS ON THE PHYSICS OF THE ABLATION/MELTING PROCESS. ONE OF THEIR WEAKEST AREAS IS THE CALCULATION OF THE HEAT ...

    SBIR Phase II 1989 Air Force Department of Defense

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