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Development of the Trident 1 aerodynamic saike mechanismThe Aerospike drag reduction mechanism was designed and developed for use on the Trident I submarine launched ballistic missile. This mechanism encounters a unique combination of environments necessitating unique design solutions to ensure satisfactory operation over its design life. The development of the Aerospike is reviewed emphasizing the unique and interesting problems encountered and their solutions.
Document ID
19790014372
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Waterman, M. D. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Richter, B. J. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Publication Information
Publication: NASA. Johnson Space Center The 13th Aerospace Mech. Symp.
Subject Category
Structural Mechanics
Accession Number
79N22543
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19790014368Collected WorksThe 13th Aerospace Mechanisms Symposium
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