Vra Inc

Company Information

Company Name
Vra Inc
Address
Po Box 50
Blacksburg, VA, 24063
Phone
n/a
URL
n/a
DUNS
n/a
Number of Employees
5

Award Totals

PROGRAM/PHASE
AWARD AMOUNT ($)
NUMBER OF AWARDS
SBIR Phase I
$359,958.00
7
SBIR Phase II
$1,015,000.00
2
Chart code to be here

Award List

  1. 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 ...

    SBIR Phase II 1985 Air ForceDepartment of Defense
  2. 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 ...

    SBIR Phase I 1984 National Aeronautics and Space Administration
  3. 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 ...

    SBIR Phase I 1985 Air ForceDepartment of Defense
  4. 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 ...

    SBIR Phase I 1984 National Aeronautics and Space Administration
  5. 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 ...

    SBIR Phase II 1988 National Aeronautics and Space Administration
  6. 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 ...

    SBIR Phase I 1987 ArmyDepartment of Defense
  7. 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 ...

    SBIR Phase I 1990 Air ForceDepartment of Defense
  8. RV BOUNDARY LAYER PLASMA

    Amount: $48,892.00

    N/A

    SBIR Phase I 1984 Air ForceDepartment of Defense
  9. HYPERSONIC PROPULSION INLETS FOR NASP APPLICATIONS

    Amount: $49,221.00

    N/A

    SBIR Phase I 1987 National Aeronautics and Space Administration

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