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Pressure Venting Tests of Phenolic Impregnated Carbon Ablator (PICA)A series of tests was devised to investigate the pressure venting behavior of one of the candidate ablators for the Orion capsule heat shield. Three different specimens of phenolic impregnated carbon ablator (PICA) were instrumented with internal pressure taps and subjected to rapid pressure changes from near vacuum to one atmosphere and simulated Orion ascent pressure histories. The specimens vented rapidly to ambient pressure and sustained no detectable damage during testing. Peak pressure differences through the thickness of a 3-inch-thick specimen were less than 1 psi during a simulated ascent pressure history.



Document ID
20160000764
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Blosser, Max L.
(NASA Langley Research Center Hampton, VA, United States)
Knutson, Jeffrey R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
January 13, 2016
Publication Date
October 1, 2015
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NF1676L-22618
L-20614
NASA-TM-2015-218965
Funding Number(s)
WBS: WBS 736466.01.08.07.31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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