Whittnghill Aerospace, LLC

Basic Information

265 Durley Avenue, Suite 208
Camarillo, CA, 93010-8544

Company Profile

n/a

Additional Details

Field Value
DUNS: 192734437
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 3


  1. Novel Propellant, High-Energy Upper Stages for Space Access

    Amount: $148,403.00

    As low-cost space access drives the design of new 3,000 lb-to-orbit launch systems, inexpensive, high-energy stages with velocity increments of over 20,000 feet/sec are required. Whittinghill Aerospac ...

    SBIR Phase I 2015 Department of Defense Defense Advanced Research Projects Agency
  2. A Modular Minimum Cost Launch System for Nano-Satellites

    Amount: $599,922.00

    As minimum cost will be required for a dedicated Nano-Sat Launch Vehicle, a parallel staged, highly modular vehicle architecture is proposed for development. The principal advantage of a modular archi ...

    SBIR Phase II 2010 National Aeronautics and Space Administration
  3. Modular NanoSat Launcher Design for Lowest Mission Cost

    Amount: $98,896.00

    As minimum cost will be required for a dedicated NanoSat Launch Vehicle, a series and parallel staged, highly modular vehicle architecture is proposed for design exploration. The principal advantage ...

    SBIR Phase I 2009 National Aeronautics and Space Administration
  4. Nitrous Oxide Liquid Injection Thrust Vector Control System Testing

    Amount: $598,953.00

    A Nitrous Oxide-fed Liquid Thrust Vector Control system is proposed as an efficient method for vehicle attitude control during powered flight. Pulled from a N2O main propulsion system oxidizer tank, i ...

    SBIR Phase II 2009 National Aeronautics and Space Administration
  5. Effectiveness of Nitrous Oxide as a Liquid Injection Thrust Vector Control Fluid

    Amount: $98,852.00

    Nitrous Oxide is proposed as an energetic liquid injection thrust vector control fluid for vehicle attitude control during dynamic vehicle maneuvers. Pulled from the main propulsion system oxidizer ta ...

    SBIR Phase I 2008 National Aeronautics and Space Administration

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