ASTROX CORP.

Address

3500 Marlbrough Way
Suite 100
College Park, MD, -

Information

DUNS: 153929260
# of Employees: 3

Ownership Information

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

Award Charts




Award Listing

  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 ...

    SBIRPhase I2012Department of Defense
  2. Rapid Design, Analysis, and Test of Hypersonic Propulsion Integrated Configurations

    Amount: $746,234.00

    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 ...

    SBIRPhase II2009Air Force Department 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 ...

    SBIRPhase I2008Air Force Department 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 ...

    SBIRPhase II2003Air Force Department 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 ...

    SBIRPhase I2002Air Force Department 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 ...

    SBIRPhase II1995Air Force Department of Defense
  7. Analysis of Off-Design Considerations for Innovative Single-Stage-to-Orbit Configurations

    Amount: $82,664.00

    N/A

    SBIRPhase I1993Air Force Department of Defense
  8. COMPUTATIONAL OPTIMIZATION OF HYPERSONIC BODIES

    Amount: $477,817.00

    N/A

    SBIRPhase II1990Air Force Department 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 ...

    SBIRPhase I1988Air Force Department of Defense
  10. COMPUTATIONAL OPTIMIZATION OF HYPERSONIC BODIES

    Amount: $49,589.00

    N/A

    SBIRPhase I1986Air Force Department of Defense

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