SBIR/STTR Research Award
Oxygen-Methane Thruster
Award amount
$50,000Program and phase
SBIR · Phase IIAward year
2007Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- Orion Propulsion, Inc.
- Proposal award date
- 2006-12-04
- Contract end date
- 2008-11-30
- UEI
- Not reported
- Solicitation number
- Not reported
- Topic code
- X7.01
Research abstract
Two main innovations will be developed in the Phase II effort that are fundamentally associated with our gaseous oxygen/gaseous methane RCS thruster. The first innovation is that of an integrated torch igniter/injector which, provides simple and reliable ignition for the thruster. The second innovation is the thruster's capability to operate with both gaseous and liquid propellants. This innovation enables greater system flexibility that is inherent in the capacity to function over a much wider range of operating conditions.
Orion has been approached by several prospective customers concerning affordable, reusable thrusters. In the current commercial market, this does not exist and the commercial sector cannot afford traditional propulsion solutions. For this reason, Orion started developing a thruster that offers the following features:
Provides an affordable solution as compared to what is currently available
Uses a different manned approach since it is reusable
Uses a modular design, which allows for the robust inspection and replacement of parts
Uses green propellants and capitalizes on in situ propellant production
Provides greater system flexibility since it operates with both liquid and gaseous propellants
Not only does the gas/gas operation of the thruster attract companies such as t/Space and Bigleow Aerospace, but its liquid/liquid operation broadens this customer base and makes this design applicable to NASA programs such as the Crew Exploration Vehicle (CEV).
Technology keywords
Not reported
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