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THERMAL CONTROL OF THE NIMBUS SPACECRAFTNimbus, in common with all contemporary spacecraft, contains an array of components and materials -- mechanical, electrical, and chemical -- which will operate effectively and reliably only when maintained in a hospitable thermal environment. Pressing existing hardware into use for space exploration, subjecting it to the rigors of outer space and possibly to uses for which it was not designed, necessitates careful thermal design to provide the proper environment.
Document ID
19630008735
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
P. Crossfield
(Goddard Space Flight Center Greenbelt, Maryland, United States)
F. Drummond
(General Electric (United States) Boston, Massachusetts, United States)
Date Acquired
August 1, 2013
Publication Date
November 14, 1962
Publication Information
Publication: Proceedings of the Nimbus Program Review
Publisher: National Aeronautics and Space Administration
URL: https://ntrs.nasa.gov/citations/19630008724
Subject Category
Space Sciences
Meeting Information
Meeting: Nimbus Program Review
Location: Valley Forge, PA
Country: US
Start Date: November 14, 1962
End Date: November 16, 1962
Sponsors: Goddard Space Flight Center
Accession Number
63N18612
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
ENVIRONMENTAL CONTROL
NIMBUS SATELLITE
THERMAL ENVIRONMENT
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