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Composite Crew Module (CCM) Permeability CharacterizationIn January 2007, the NASA Administrator chartered the NASA Engineering and Safety Center (NESC) to form an Agency team to design and build a composite crew module in 18 months in order to gain hands-on experience in anticipation that future exploration systems may be made of composite materials. One of the conclusions from this Composite Crew Module Primary Structure assessment was that there was a lack of understanding regarding the ability for composite pressure shells to contain consumable gases, which posed a technical risk relative to the use of a metallic design. After the completion of the Composite Crew Module test program, the test article was used in a new program to assess the overall leakage/permeability and identify specific features associated with high leak rates. This document contains the outcome of the leakage assessment.
Document ID
20130013592
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Kirsch, Michael T.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 27, 2013
Publication Date
May 1, 2013
Subject Category
Space Transportation And Safety
Report/Patent Number
NASA/TM-2013-217990
L-20258
NESC-RP-10-00685
NF1676L-16612
Report Number: NASA/TM-2013-217990
Report Number: L-20258
Report Number: NESC-RP-10-00685
Report Number: NF1676L-16612
Funding Number(s)
WBS: WBS 869021.05.07.07.29
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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