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Trade Study of Multiple Thruster Options for the Mars Airplane ConceptA trade study was performed at NASA Langley Research Center under the Planetary Airplane Risk Reduction (PARR) project (2004-2005) to examine the option of using multiple, smaller thrusters in place of a single large thruster on the Mars airplane concept with the goal to reduce overall cost, schedule, and technical risk. The 5-lbf (22N) thruster is a common reaction control thruster on many satellites. Thousands of these types of thrusters have been built and flown on numerous programs, including MILSTAR and Intelsat VI. This study has examined the use of three 22N thrusters for the Mars airplane propulsion system and compared the results to those of the baseline single thruster system.
Document ID
20090013835
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Kuhl, Christopher A.
(NASA Langley Research Center Hampton, VA, United States)
Gayle, Steven W.
(NASA Langley Research Center Hampton, VA, United States)
Hunter, Craig A.
(NASA Langley Research Center Hampton, VA, United States)
Kenney, Patrick S.
(NASA Langley Research Center Hampton, VA, United States)
Scola, Salvatore
(NASA Langley Research Center Hampton, VA, United States)
Paddock, David A.
(NASA Langley Research Center Hampton, VA, United States)
Wright, Henry S.
(NASA Langley Research Center Hampton, VA, United States)
Gasbarre, Joseph F.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
March 1, 2009
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
L-19371
LF99-5349
NASA/TM-2009-215699
Report Number: L-19371
Report Number: LF99-5349
Report Number: NASA/TM-2009-215699
Funding Number(s)
WBS: WBS 698671.02.07.02.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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