Vra Inc

Company Information
Address Po Box 50
Blacksburg, VA, 24063


Information

DUNS:

# of Employees: 5


Ownership Information

HUBZone Owned: N

Socially and Economically Disadvantaged: N

Woman Owned: N



Award Charts




Award Listing

  1. LOW-TO-HIGH ALTITUDE NONEQUILIBRIUM VSL/PNS SCHEME FOR BRV/MARV/DECOY APPLICATIONS

    Amount: $53,181.00

    BECAUSE OF A LACK OF ADEQUATE FLIGHT OR GROUND TEST DATA FOR HYPERSONIC REENTRY CONDITIONS, THE DESIGN AND ANALYSIS OF EXISTING AND FUTURE BRVS, MARVS AND DECOYS WILL INCREASINGLY BENEFIT FROM THE DEV ...

    SBIRPhase I1990Air Force Department of Defense
  2. HYPERSONIC PROPULSION INLETS FOR NASP APPLICATIONS

    Amount: $485,000.00

    OVER THE PAST SEVERAL YEARS, IT HAS BEEN CLEARLY DEMONSTRATED THAT DEVELOPMENT OF TRANSATMOSPHERIC VEHICLES, SUCH AS THE NATIONAL AEROSPACE PLANE (NASP), WILL BE NECESSARY FOR A SUCCESSFUL SPACE-DEFEN ...

    SBIRPhase II1988National Aeronautics and Space Administration
  3. HYPERSONIC PROPULSION INLETS FOR NASP APPLICATIONS

    Amount: $49,221.00

    N/A

    SBIRPhase I1987National Aeronautics and Space Administration
  4. FINITE DIFFERENCE FLOW CALCULATIONS FOR HELICOPTER ROTOR/FUSELAGE CONFIGURATIONS

    Amount: $58,750.00

    THE DEVELOPMENT OF A COMPUTER CODE TO SOLVE FOR THE FLOW OVER A HELICOPTER ROTOR/FUSELAGE CONFIGURATION IS PROPOSED. A MODULAR APPROACH IS TO BE USED WHERE TWO EXISTING FINITE DIFFERENCE CODES, ONE FO ...

    SBIRPhase I1987Army Department of Defense
  5. RV BOUNDARY LAYER PLASMA

    Amount: $530,000.00

    CARBON, EPOXY AND TEFLON ARE SOME OF THE MOST COMMON AND FREQUENTLY USED MATERIALS FOR RV APPLICATIONS. UNDER HYPERSONIC REENTRY CONDITIONS AT HIGH ANGLES OF ATTACK THE ABLATION PRODUCTS FROM THESE MA ...

    SBIRPhase II1985Air Force Department of Defense
  6. OVER THE PAST SEVERAL YEARS SIGNIFICANT INTEREST HAS BEEN GENERATED IN THREE-DIMENSIONAL FLOWFIELD ANALYSES OF LIFTING REENTRY VEHICLES.

    Amount: $49,975.00

    OVER THE PAST SEVERAL YEARS SIGNIFICANT INTEREST HAS BEEN GENERATED IN THREE-DIMENSIONAL FLOWFIELD ANALYSES OF LIFTING REENTRY VEHICLES. THE PARABOLIZED NAVIER-STOKES (PNS) SCHEMES ARE ELLIPTIC IN THE ...

    SBIRPhase I1985Air Force Department of Defense
  7. ALTITUDES

    Amount: $49,946.00

    IN ORDER TO OPTIMIZE THE APPLICATION OF AEROASSIST CONCEPTS TO MANEUVERING RE-ENTRY VEHICLES, IT IS ESSENTIAL TO HAVE A SCHEME THAT CAN ACCURATELY AND SIMULTANEOUSLY PREDICT THE VEHICLE'S AERODYNAMIC ...

    SBIRPhase I1984National Aeronautics and Space Administration
  8. REENTRY

    Amount: $49,993.00

    IN RECENT YEARS THE PROJECTED DESIGN OF ADVANCED ORBITAL TRANSFER VEHICLES HAS BEEN EVOLVING VERY RAPIDLY. THESE VEHICLES ARE TO OPERATE AND DECELERATE IN THE LOW-DENSITY (HIGH-ALTITUDE) FLIGHT REGIME ...

    SBIRPhase I1984National Aeronautics and Space Administration
  9. RV BOUNDARY LAYER PLASMA

    Amount: $48,892.00

    N/A

    SBIRPhase I1984Air Force Department of Defense

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