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Orion Spacecraft MMOD Protection Design and AssessmentThe Orion spacecraft will replace the Space Shuttle Orbiter for American and international partner access to the International Space Station by 2015 and, afterwards, for access to the moon for initial sorties and later for extend outpost visits as part of the Constellation Exploration Initiative. This work describes some of the efforts being undertaken to ensure that Orion design will meet or exceed the stringent MicroMeteoroid and Orbital Debris (MMOD) requirements set out by NASA when exposed to the environments encountered with these missions. This paper will provide a brief overview of the approaches being used to provide MMOD protection to the Orion vehicle and to assess the spacecraft for compliance to the Constellation Program s MMOD requirements.
Document ID
20090024215
Acquisition Source
Johnson Space Center
Document Type
Extended Abstract
Authors
Bohl, William
(Lockheed Martin Space Systems Co. Denver, CO, United States)
Miller, Joshua
(Lockheed Martin Space Systems Co. Denver, CO, United States)
Deighton, Kevin
(Lockheed Martin Corp. Houston, TX, United States)
Foreman, Cory
(Lockheed Martin Corp. Houston, TX, United States)
Yasensky, John
(Lockheed Martin Corp. Houston, TX, United States)
Christiansen, Eric
(NASA Johnson Space Center Houston, TX, United States)
Hyde, James
(NASA Johnson Space Center Houston, TX, United States)
Nahra, Henry
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2009
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JSC-CN-18500
Report Number: JSC-CN-18500
Meeting Information
Meeting: 11th Hypervelocity Impact Symposium
Location: Freiburg
Country: Germany
Start Date: April 11, 2010
End Date: April 15, 2010
Sponsors: Hypervelocity Impact Society
Distribution Limits
Public
Copyright
Public Use Permitted.
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