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Compression-Spring Separation MechanismsThe separation of spacecraft components, which occur in every flight, represents crucial and major events that must be successfully executed to fulfill mission requirements. Separation systems vary as widely in physical and functional properties as the performance requirements which they must satisfy; however, most systems use helical compression springs as an energy source. This paper summarizes the principal design characteristics of separation mechanisms and empirical data obtained from actual separations in space.
Document ID
19660027413
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
T G Harrington
(Lockheed Missiles and Space Company Sunnyvale, CA, United States)
Date Acquired
August 3, 2013
Publication Date
May 19, 1966
Publication Information
Publication: Proceedings of the First Aerospace Mechanisms Symposium
Publisher: U. S. Department of Commerce
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-77971
Meeting Information
Meeting: 1st Aerospace Mechanisms Symposium
Location: Santa Clara, CA
Country: US
Start Date: May 19, 1966
End Date: May 20, 1966
Sponsors: Lockheed Martin (United States), Jet Propulsion Lab
Accession Number
66N36703
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SHROUD
SPACECRAFT COMPONENT
SPRING
SEPARATION
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