Orion Pad Abort 1 Crew Module mass properties test approach and results /

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Bibliographic Details
Author / Creator:Herrera, Claudia, author.
Imprint:Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, 2012.
Description:1 online resource (23 pages) : illustrations (some color).
Language:English
Series:NASA/TM ; 2012-215995
NASA technical memorandum ; 2012-215995.
Subject:
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/9142787
Hidden Bibliographic Details
Other authors / contributors:Harding, Adam, author.
Hugh L. Dryden Flight Research Center issuing body.
Notes:Title from title screen (viewed on June 17, 2013).
"March 2012."
Includes bibliographical references (page 23).
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:2012-215995

MARC

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650 7 |a Crew Exploration Vehicle.  |2 nasat 
650 7 |a Launching pads.  |2 nasat 
650 7 |a Aborted missions.  |2 nasat 
650 7 |a SPACECRAFT MODULES.  |2 nasat 
650 7 |a Flight tests.  |2 nasat 
650 7 |a Mass distribution.  |2 nasat 
650 7 |a Aerodynamic loads.  |2 nasat 
650 7 |a Moments of inertia.  |2 nasat 
650 7 |a Dynamic structural analysis.  |2 nasat 
650 7 |a Moments of inertia.  |2 fast  |0 http://id.worldcat.org/fast/fst01025015 
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