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Structural Integrity and Durability of Reusable Space Propulsion SystemsA two-day conference on the structural integrity and durability of reusable space propulsion systems was held on 14 to 15 May 1991 at the NASA Lewis Research Center. Presentations were made by industry, university, and government researchers organized into four sessions: (1) aerothermodynamic loads; (2) instrumentation; (3) fatigue, fracture, and constitutive modeling; and (4) structural dynamics. The principle objectives were to disseminate research results and future plans in each of four areas. This publication contains extended abstracts and the visual material presented during the conference. Particular emphasis is placed on the Space Shuttle Main Engine (SSME) and the SSME turbopump.
Document ID
19930022363
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Date Acquired
September 6, 2013
Publication Date
May 1, 1991
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.55:10064
E-6068
NASA-CP-10064
Report Number: NAS 1.55:10064
Report Number: E-6068
Report Number: NASA-CP-10064
Accession Number
93N31552
Funding Number(s)
PROJECT: RTOP 553-13-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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