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Advanced Chemical Propulsion for Science MissionsThe advanced chemical propulsion technology area of NASA's In-Space Technology Project is investing in systems and components for increased performance and reduced cost of chemical propulsion technologies applicable to near-term science missions. Presently the primary investment in the advanced chemical propulsion technology area is in the AMBR high temperature storable bipropellant rocket engine. Scheduled to be available for flight development starting in year 2008, AMBR engine shows a 60 kg payload gain in an analysis for the Titan-Enceladus orbiter mission and a 33 percent manufacturing cost reduction over its baseline, state-of-the-art counterpart. Other technologies invested include the reliable lightweight tanks for propellant and the precision propellant management and mixture ratio control. Both technologies show significant mission benefit, can be applied to any liquid propulsion system, and upon completion of the efforts described in this paper, are at least in parts ready for flight infusion. Details of the technologies are discussed.
Document ID
20080014199
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Liou, Larry
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
March 1, 2008
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-16298
NASA/TM-2008-215069
AIAA Paper 1482
Report Number: E-16298
Report Number: NASA/TM-2008-215069
Report Number: AIAA Paper 1482
Meeting Information
Meeting: 2008 IEEE Aerodpace Conference
Location: Big Sky, MT
Country: United States
Start Date: March 1, 2008
End Date: March 8, 2008
Sponsors: Institute of Electrical and Electronics Engineers, American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 346620.01.03.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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