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Fly-away restraint pin mechanism for the Army's PATRIOT missile systemThe development of the longitudinal restraint mechanism for the PATRIOT missile system is reviewed. Two approaches for the restraint pin design are discussed: an initial ordnance mechanism, and a passive fly-away mechanism. Because of reliability problems and a desire to reduce cost the fly-away restraint mechanism was chosen.
Document ID
19780011087
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Knight, F. W. (Martin Marietta Aerospace Denver, CO, United States)
Date Acquired
August 9, 2013
Publication Date
April 1, 1977
Publication Information
Publication: NASA. Goddard Res. Center The 11th Aerospace Mech. Symp.
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
78N19030
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19780011083Collected WorksThe 11th Aerospace Mechanisms Symposium
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