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Structural evaluation of deployable aerodynamic spike boomsAn extendable boom consisting of a series of telescopic cylindrical tube segments and overlapping lock joints developed for use as an aerodynamic spike mounted atop a missile is described. Two candidate design concepts differing mainly in the particular overlapping lock joint designs are undergoing a combined analytical/experimental evaluation. Some of the results of this evaluation are presented.
Document ID
19760012087
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Richter, B. J. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1975
Publication Information
Publication: NASA. Kennedy Space Center 9th Aerospace Mech. Symp.
Subject Category
Spacecraft Instrumentation
Accession Number
76N19175
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19760012084Collected WorksThe 9th Aerospace Mechanisms Symposium19760012084Collected WorksThe 9th Aerospace Mechanisms Symposium
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