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Company Information:

Company Name:
Whittnghill Aerospace, LLC
Address:
265 Durley Avenue, Suite 208
Camarillo, CA 93010-8544
Phone:
(805) 901-2297
URL:
N/A
EIN:
134295273
DUNS:
192734437
Number of Employees:
3
Woman-Owned?:
No
Minority-Owned?:
No
HUBZone-Owned?:
No

Commercialization:

Has been acquired/merged with?:
N/A
Has had Spin-off?:
N/A
Has Had IPO?:
N/A
Year of IPO:
N/A
Has Patents?:
N/A
Number of Patents:
N/A
Total Sales to Date $:
$ 0.00
Total Investment to Date $
$ 0.00
POC Title:
N/A
POC Name:
N/A
POC Phone:
N/A
POC Email:
N/A
Narrative:
N/A

Award Totals:

Program/Phase Award Amount ($) Number of Awards
SBIR Phase I $197,748.00 2
SBIR Phase II $1,198,875.00 2

Award List:

Effectiveness of Nitrous Oxide as a Liquid Injection Thrust Vector Control Fluid

Award Year / Program / Phase:
2008 / SBIR / Phase I
Award Amount:
$98,852.00
Agency:
NASA
Principal Investigator:
George Whittinghill, Principal Investigator
Abstract:
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… More

Modular NanoSat Launcher Design for Lowest Mission Cost

Award Year / Program / Phase:
2009 / SBIR / Phase I
Award Amount:
$98,896.00
Agency:
NASA
Principal Investigator:
George Whittinghill, Principal Investigator
Abstract:
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… More

Nitrous Oxide Liquid Injection Thrust Vector Control System Testing

Award Year / Program / Phase:
2009 / SBIR / Phase II
Award Amount:
$598,953.00
Agency:
NASA
Principal Investigator:
George Whittinghill, Principal Investigator
Abstract:
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… More

A Modular Minimum Cost Launch System for Nano-Satellites

Award Year / Program / Phase:
2010 / SBIR / Phase II
Award Amount:
$599,922.00
Agency:
NASA
Principal Investigator:
George Whittinghill, Principal Investigator
Abstract:
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… More