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A Versatile Drop Test Procedure for the Simulation of Impact EnvironmentsIn order to assure the reliability of space flight systems and spacecraft, it is necessary to subject these systems, vehicles, and their components to expected shock and impact environmental loads. The Langley Laboratory has found the apparatus and methods discussed in this paper useful in its work along these lines, and feels that other organizations might also find them of value.
Document ID
19620003679
Acquisition Source
Headquarters
Document Type
Reprint (Version printed in journal)
Authors
George W Brooks
(Langley Research Center Hampton, Virginia, United States)
Huey D Carden
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
August 1, 2013
Publication Date
September 1, 1961
Publication Information
Publication: Noise Control
Publisher: Acoustical Society of America
Volume: 7
Issue: 5
Issue Publication Date: September 1, 1961
Subject Category
Structural Mechanics
Accession Number
62N13679
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Impact
Environment simulation
Simulation
Drop test
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