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Whittinghill Aerospace

Company Information
Address
265 Durley Ave, Ste 213
camarillo, CA 93010-8526
United States



Information

UEI: U57KL1KQM3L8

# of Employees: 3


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: No



Award Charts




Award Listing

  1. Novel Propellant, High-Energy Upper Stage Development

    Amount: $979,798.94

    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 ...

    SBIRPhase II2017Department of Defense Defense Advanced Research Projects Agency
  2. Novel Propellant, High-Energy Upper Stages for Space Access

    Amount: $148,402.88

    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 ...

    SBIRPhase I2015Department of Defense Defense Advanced Research Projects Agency
  3. 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 ...

    SBIRPhase II2010National Aeronautics and Space Administration
  4. 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 ...

    SBIRPhase I2009National Aeronautics and Space Administration
  5. 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 ...

    SBIRPhase II2009National Aeronautics and Space Administration
  6. 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 ...

    SBIRPhase I2008National Aeronautics and Space Administration
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