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Mount mechanisms for the Saturn 5/Apollo mobile launcher at John F. Kennedy Space CenterA support system was designed to resist hurricane wind loads at the launch pad and to allow the supported structural frame to expand and contract freely under wide ranges of temperature. This system consists of six mount mechanisms devised to meet the previously stated requirements plus a load-carrying capacity for each of 3.2-million kilograms (7-million pounds) downward and 1.6-million kilograms (3.5-million pounds) upward. A similar but lighter system of six mount mechanisms was designed for use in the sheltered environment of the vehicle assembly building. Each requirement and design result is discussed, and each mount mechanism is defined by location and type with references to visual presentations.
Document ID
19760012109
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Balke, H. A.
(Balke (Harry A.) Engineers Cincinnati, OH, 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
Ground Support Systems And Facilities (Space)
Accession Number
76N19197
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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