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Cryogenics for spacecraftIt is pointed out that cryogenic engineering has been an integral part of space research almost from the beginning of the space age because of the significant performance advantages available from cryogenically fueled rocket engines. In recent years, space-related cryogenic engineering has expanded from booster engines to include spacecraft systems because of the vastly improved performance available from cooled detectors and systems. The requirements for detector cooling in space are examined, taking into account earth observation, atmospheric measurements, infrared astronomy, X-ray astronomy, gamma-ray astronomy, radio astronomy, relativity measurements, magnetic field measurements, time measurements, and data processing. A description is presented of 1978-1981 U.S. spacecraft cryogenic detector systems.
Document ID
19790046989
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Vorreiter, J. W.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Spacecraft Instrumentation
Meeting Information
Meeting: ICEC 7; Seventh International Cryogenic Engineering Conference
Location: London
Start Date: July 4, 1978
End Date: July 7, 1978
Accession Number
79A31002
Distribution Limits
Public
Copyright
Other

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