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Design and development of the redundant launcher stabilization system for the Atlas 2 launch vehicleThe Launcher Stabilization System (LSS) is a pneumatic/hydraulic ground system used to support an Atlas launch vehicle prior to launch. The redesign and development activity undertaken to achieve an LSS with increased load capacity and a redundant hydraulic system for the Atlas 2 launch vehicle are described.
Document ID
19910015293
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nakamura, M. (General Dynamics Corp. San Diego, CA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1991
Publication Information
Publication: JPL, The 25th Aerospace Mechanisms Symposium
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
91N24607
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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