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TRIDENT 1 third stage motor separation systemThe third stage engine separation system has shown through test and analysis that it can effectively and reliably perform its function. The weight of the hardware associated with this system is well within the targeted value.
Document ID
19790013213
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Welch, B. H. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Richter, B. J. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Sue, P. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 9, 2013
Publication Date
April 28, 1977
Publication Information
Publication: NASA. Goddard Space Flight Center The 11th Aerospace Mech. Symp.
Subject Category
Mechanical Engineering
Accession Number
79N21384
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19790013203Collected WorksThe 11th Aerospace Mechanisms Symposium
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