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Design, Integration, Certification and Testing of the Orion Crew Module Propulsion SystemThe Orion Crew Module Propulsion Reaction Control System is currently complete and ready for flight as part of the Orion program's first flight test, Exploration Flight Test One (EFT-1). As part of the first article design, build, test, and integration effort, several key lessons learned have been noted and are planned for incorporation into the next build of the system. This paper provides an overview of those lessons learned and a status on the Orion propulsion system progress to date.
Document ID
20140009924
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
McKay, Heather (Lockheed Martin Space Systems Co. Houston, TX, United States)
Coffman, Eric (Lockheed Martin Space Systems Co. Houston, TX, United States)
May, Sarah (Lockheed Martin Space Systems Co. Houston, TX, United States)
Freeman, Rich (Lockheed Martin Space Systems Co. Houston, TX, United States)
Cain, George (Lockheed Martin Space Systems Co. Houston, TX, United States)
Albright, John (NASA Johnson Space Center Houston, TX, United States)
Schoenberg, Rich (NASA Johnson Space Center Houston, TX, United States)
Delventhal, Rex (NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
July 21, 2014
Publication Date
July 28, 2014
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
JSC-CN-31424
Meeting Information
Meeting: AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Location: Cleveland, OH
Country: United States
Start Date: July 28, 2014
End Date: July 30, 2014
Sponsors: American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers, Society of Automotive Engineers, Inc., American Society for Electrical Engineers
Funding Number(s)
CONTRACT_GRANT: NNJ06TA25C
Distribution Limits
Public
Copyright
Public Use Permitted.

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