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ASTROX CORP
UEI: G7DBH38ZAEQ8
# of Employees: 3
HUBZone Owned: No
Socially and Economically Disadvantaged: Yes
Woman Owned: No
Award Charts
Award Listing
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Micro Scale Testing of High Speed Aircraft
Amount: $149,948.00ABSTRACT: 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 Air Force -
Rapid Design, Analysis, and Test of Hypersonic Propulsion Integrated Configurations
Amount: $746,234.00The 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 II2009Department of Defense Air Force -
Rapid Design, Analysis, and Test of Hypersonic Propulsion Integrated Configurations
Amount: $99,456.00The 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 I2008Department of Defense Air Force -
Flow Analysis Software Tool- SuperSIDE
Amount: $749,494.00The 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 II2003Department of Defense Air Force -
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 I2002Department of Defense Air Force -
Analysis of Off-Design Considerations for Innovative Single-Stage-to-Orbit Configurations
Amount: $494,509.00An 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 II1995Department of Defense Air Force -
Analysis of Off-Design Considerations for Innovative Single-Stage-to-Orbit Configurations
Amount: $82,664.00N/A
SBIRPhase I1993Department of Defense Air Force -
COMPUTATIONAL OPTIMIZATION OF HYPERSONIC BODIES
Amount: $477,817.00N/A
SBIRPhase II1990Department of Defense Air Force -
RAREFIELD GAS FLOW EFFECTS ON HYPERSONIC VEHICLES
Amount: $47,823.00BASED 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 I1988Department of Defense Air Force -
COMPUTATIONAL OPTIMIZATION OF HYPERSONIC BODIES
Amount: $49,589.00N/A
SBIRPhase I1986Department of Defense Air Force