Whittnghill Aerospace, LLC

265 Durley Avenue, Suite 208
Camarillo, CA 93010

SBIR Award Summary

Total Number of Awards 5
Total Value of Awards $1.55MM
First Award Date 01/01/08
Most Recent Award Date 09/29/15

Key Personnel

Last Name Name Awards Contact
Whittinghill George Whittinghill 4 Message
Whittinghill George Whittinghill 2 Message

5 Awards Won

Phase 1 SBIR

Agency: Defense Advanced Research Projects Agency
Topic: SB152-008
Budget: 09/29/15 - 06/30/16

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 Aerospace proposes development of a highly energetic stage design for DARPA?s XS-1 launch vehicle that makes use of novel propellants and a high mass fract...

Phase 2 SBIR

Agency: National Aeronautics and Space Administration
Topic: 10-2-S4
Budget: 01/01/10 - 12/31/10

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 architecture for this size of vehicle is the single propulsion development for the boost stages at a relatively small scale. This approach drastically ...

Phase 2 SBIR

Agency: National Aeronautics and Space Administration
Topic: 09-2
Budget: 01/01/09 - 12/31/09

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, it features system simplicity, no toxicity, room temperature storability, high system mass fraction and superior performance due to its exothermic d...

Phase 1 SBIR

Agency: National Aeronautics and Space Administration
Topic: 09-1
Budget: 01/01/09 - 12/31/09

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 of a modular architecture on this size vehicle is a single propulsion development at a relatively small scale which drastically shortens developmen...

Phase 1 SBIR

Agency: National Aeronautics and Space Administration
Topic: 08-1
Budget: 01/01/08 - 12/31/08

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 tank, it features system simplicity, no toxicity, room temperature storability, high system mass fraction and superior performance due to its exother...