ASTROX CORP.

Basic Information

3500 Marlbrough Way
Suite 100
College Park, MD, -

Company Profile

n/a

Additional Details

Field Value
DUNS: 153929260
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 3


  1. Micro Scale Testing of High Speed Aircraft

    Amount: $149,948.00

    ABSTRACT: The Air Force has the need to advance high speed vehicle technology and experimental flight test methods quickly and cheaply. Heretofore, the Air Force test programs have consumed too much ...

    SBIR Phase I 2012 Department of DefenseAir ForceDepartment of Defense
  2. Rapid Design, Analysis, and Test of Hypersonic Propulsion Integrated Configurations

    Amount: $749,234.00

    The Air Force Research Laboratory Air Vehicles Directorate needs to be able to rapidly develop hypersonic vehicle concepts and to do so with as little risk as possible. A new technology called Rapid P ...

    SBIR Phase II 2009 Air ForceDepartment of DefenseDepartment of Defense
  3. Rapid Design, Analysis, and Test of Hypersonic Propulsion Integrated Configurations

    Amount: $99,456.00

    The Air Force Research Laboratory Air Vehicles Directorate needs to be able to rapidly develop hypersonic vehicle concepts and to do so with as little risk as possible. A new technology called Rapid P ...

    SBIR Phase I 2008 Air ForceDepartment of DefenseDepartment of Defense
  4. Flow Analysis Software Tool- SuperSIDE

    Amount: $749,494.00

    The need for innovative combined cycle engines for Space Access and hypersonic vehicles leads the Air Force design engineers to the requirement for analysis tools that provide higher levels of fidelit ...

    SBIR Phase II 2003 Air ForceDepartment of DefenseDepartment of Defense
  5. Combined-Cycle Engine Flow Path Analysis & Design Software Tool

    Amount: $99,895.00

    "The need for innovative combined cycle engines for Space Access and hypersonicvehicles leads the Air Force design engineers to the requirement for analysistools that provide higher levels of fidelity ...

    SBIR Phase I 2002 Air ForceDepartment of DefenseDepartment of Defense
  6. Analysis of Off-Design Considerations for Innovative Single-Stage-to-Orbit Configurations

    Amount: $494,509.00

    An existing hypersonic vehicle design code predicts EISP performance increases of 200-400 seconds over traditional single-stage-to-orbit configurations. If realized, such increase may have profound ef ...

    SBIR Phase II 1995 Air ForceDepartment of DefenseDepartment of Defense
  7. Analysis of Off-Design Considerations for Innovative Single-Stage-to-Orbit Configurations

    Amount: $82,664.00

    N/A

    SBIR Phase I 1993 Air ForceDepartment of DefenseDepartment of Defense
  8. COMPUTATIONAL OPTIMIZATION OF HYPERSONIC BODIES

    Amount: $477,817.00

    N/A

    SBIR Phase II 1990 Air ForceDepartment of DefenseDepartment of Defense
  9. RAREFIELD GAS FLOW EFFECTS ON HYPERSONIC VEHICLES

    Amount: $47,823.00

    BASED UPON A PRELIMINARY LITERATURE SEARCH, SEVERAL POSSIBLE AREAS FOR FUTURE RESEARCH WERE IDENTIFIED. FIRST, THERE APPEARS TO BE NO PUBLISHED IDENTIFICATION OF THE RAREFIELD FLOW REGIMES, AND CRUCIA ...

    SBIR Phase I 1988 Air ForceDepartment of DefenseDepartment of Defense
  10. COMPUTATIONAL OPTIMIZATION OF HYPERSONIC BODIES

    Amount: $49,589.00

    N/A

    SBIR Phase I 1986 Air ForceDepartment of DefenseDepartment of Defense

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