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High Performance Bipropellant Space Engines

Award Information

Agency:
National Aeronautics and Space Administration
Branch:
N/A
Award ID:
83839
Program Year/Program:
2007 / SBIR
Agency Tracking Number:
066580
Solicitation Year:
N/A
Solicitation Topic Code:
N/A
Solicitation Number:
N/A
Small Business Information
Plasma Processes LLC.
4914 Moores Mill Road Huntsville, AL 35811-1558
View profile »
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: Yes
 
Phase 1
Fiscal Year: 2007
Title: High Performance Bipropellant Space Engines
Agency: NASA
Contract: NNJ07JB06C
Award Amount: $100,000.00
 

Abstract:

Advanced bipropellant engines are needed for ARES/ORION vehicle maneuvering and future deep space science missions. Currently, an iridium-lined rhenium combustion chamber is the state-of-the-art for in-space propulsion applications. An example of an in-space engine that incorporates an iridium-lined rhenium thruster is Aerojet's HiPAT apogee engine. This engine uses monomethyl-hydrazine (MMH, CH3N2H3) as fuel and nitrogen tetroxide (N2O4, specifically MON-3) as oxidizer. To increase performance of bipropellant engines, improved chamber materials are needed that will allow higher operating conditions (pressure and temperature) and better resistance to oxidation. Therefore, Plasma Processes, Inc. and its partner, Aerojet, propose to develop hafnium oxide-iridium lined rhenium combustion chambers that will simplify engine design and allow higher operating conditions. As a result, a lower cost, higher performance bipropellant space engine will be produced.

Principal Investigator:

John S. O'Dell
Principal Investigator
2568517653
scottodell@plasmapros.com

Business Contact:

Timothy N. McKechnie
President
2568517653
timmck@plasmapros.com
Small Business Information at Submission:

Plasma Processes, Inc.
4914 Moores Mill Road Huntsville, AL 35811

EIN/Tax ID: 631100320
DUNS: N/A
Number of Employees:
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No