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Space shuttle separation mechanismsThe development of space shuttle separation devices is reviewed to illustrate the mechanisms involved in separating the Orbiter from the Boeing 747 carrier aircraft and from the externally mounted propellant tank. Other aspects of the separation device development discussed include design evolution, operational experience during the orbiter approach and landing tests, and the work required to produce an operational system.
Document ID
19780024234
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Rogers, W. F.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1978
Subject Category
Space Transportation
Report/Patent Number
NASA-TM-58210
Accession Number
78N32177
Funding Number(s)
PROJECT: RTOP 953-36-00-00-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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