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The Surveyor Thermal SwitchThe extemal temperatme extremes of the lunar swjace dictated that a means be found to control the two electronic compartments on the Surveyot soft lunar landing vehicle within a narrower temperatme band to assure satisfactory component pmjonnance. Accordingly, thermal switches were developed to conduct heat away from temperature-sensitive components while heat-generating components were operating during the lunar day, and to retain heat at night when the equipment was off.

Future equipment required to vary thermal conductivities, should this principle be employed, can benefit greatly from the results of the many problems encountered and studies made.
Document ID
19670026886
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
Authors
T E Deal
(Hughes Aircraft (United States) Los Angeles, United States)
Date Acquired
August 3, 2013
Publication Date
August 15, 1967
Subject Category
Space Vehicles
Meeting Information
Meeting: 2nd Aerospace Mechanisms Symposium
Location: Santa Clara, CA
Country: US
Start Date: May 4, 1967
End Date: May 5, 1967
Sponsors: National Aeronautics and Space Administration, Jet Propulsion Laboratory
Accession Number
67N36215
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LUNAR SURFACE
SURVEYOR SPACECRAFT
SWITCH
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