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Hydroburst test of a carbon-carbon involute exit coneA hydroburst test of the aft portion of the PAM-D exit cone and the test procedure are described in detail. The hydrostatic pressure required to buckle the cone was 9.75 psi. Meanwhile, the PAM-D exit cone was modeled using the finite element method and a theoretical bucking pressure (8.76 psi) was predicted using the SPAR finite element code. The modeling technique employed is discussed. By comparing the theoretical to predicted critical pressures, this report verifies the modeling technique and calculates a material knockdown factor for the carbon-carbon exit cone.
Document ID
19880004730
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Sullivan, Roy M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NAS 1.60:2556
NASA-TP-2556
Report Number: NAS 1.60:2556
Report Number: NASA-TP-2556
Accession Number
88N14112
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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