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Bonding and Sealing Evaluations for Cryogenic TanksSeveral different cryogenic tank concepts are being considered for reusable launch vehicles (RLV'S) . Though different tank concepts are being considered, many will require that the cryogenic insulation be evacuated and be bonded to a structure. In this work, an attempt was made to evaluate the effectiveness of maintaining a vacuum on a specimen where foam or honeycomb core was encased within Gr/Ep. In addition to these tests, flatwise adhesion pull off tests were performed at room temperature with PR 1664, EA 9394, FM-300, Crest 3170, and HT 435 adhesives. The materials bonded included Gr/Ep, Gr/BMI, Al, and stainless steel facesheets, and Ti honeycomb, Hexcel honeycomb, and Rohacell foam core materials.
Document ID
19970029012
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Glass, David E.
(Analytic Services and Materials, Inc. Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1997
Subject Category
Nonmetallic Materials
Report/Patent Number
ASM-LS05-97-01
NAS 1.26:201734
NASA-CR-201734
Report Number: ASM-LS05-97-01
Report Number: NAS 1.26:201734
Report Number: NASA-CR-201734
Accession Number
97N27720
Funding Number(s)
PROJECT: RTOP 242-33-01
CONTRACT_GRANT: NAS1-96014
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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