HYPERSONICS

Address

164 FERNE COURT
PALO ALTO, CA, 94306 0460

Information

DUNS: 178051900
# of Employees: 4

Ownership Information

Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N

Award Charts




Award Listing

  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 ...

    SBIRPhase II2006Air 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 ...

    SBIRPhase I2005Air Force Department of Defense
  3. Unitary Numerical Method For Flow And Heatshield Analysis

    Amount: $69,904.00

    N/A

    SBIRPhase I1995National Aeronautics and Space Administration
  4. RF Performance Measurements in Simulated Reentry Environments

    Amount: $72,789.00

    N/A

    SBIRPhase I1993Air Force Department of Defense
  5. Development of Base-Flow Computer Code

    Amount: $63,000.00

    N/A

    SBIRPhase I1993Air 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 ...

    SBIRPhase II1992National 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 ...

    SBIRPhase II1991Air Force Department of Defense
  8. INNOVATIVE MODEL FOR REACTING FLOWS

    Amount: $48,662.00

    N/A

    SBIRPhase I1991National Aeronautics and Space Administration
  9. ADVANCED AEROTHERMOCHEMISTRY ALGORITHM

    Amount: $69,743.00

    N/A

    SBIRPhase I1990Air 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 ...

    SBIRPhase II1989Air Force Department of Defense

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