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Whittinghill Aerospace
UEI: U57KL1KQM3L8
# of Employees: 3
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: No
Award Charts
Award Listing
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Novel Propellant, High-Energy Upper Stage Development
Amount: $979,798.94As 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 -
Novel Propellant, High-Energy Upper Stages for Space Access
Amount: $148,402.88As 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 -
A Modular Minimum Cost Launch System for Nano-Satellites
Amount: $599,922.00As 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 -
Modular NanoSat Launcher Design for Lowest Mission Cost
Amount: $98,896.00As 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 -
Nitrous Oxide Liquid Injection Thrust Vector Control System Testing
Amount: $598,953.00A 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 -
Effectiveness of Nitrous Oxide as a Liquid Injection Thrust Vector Control Fluid
Amount: $98,852.00Nitrous 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