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Contamination control program for the Cosmic Background Explorer: An overviewEach of the three state of the art instruments flown aboard NASA's Cosmic Background Explorer (COBE) were designed, fabricated, and integrated using unique contamination control procedures to ensure accurate characterization of the diffuse radiation in the universe. The most stringent surface level cleanliness specifications ever attempted by NASA were required by the Diffuse Infrared Background Experiment (DRIBE) which is located inside a liquid helium cooled dewar along with the Far Infrared Absolute Spectrophotometer (FIRAS). The DRIBE instrument required complex stray radiation suppression that defined a cold primary optical baffle system surface cleanliness level of 100A. The cleanliness levels of the cryogenic FIRAS instrument and the Differential Microwave Radiometer (DMR) which were positioned symmetrically around the dewar were less stringent ranging from 300 to 500A. To achieve these instrument cleanliness levels, the entire flight spacecraft was maintained at level 500A throughout each phase of development. The COBE contamination control program is described along with the difficulties experienced in maintaining the cleanliness quality of personnel and flight hardware throughout instrument assembly.
Document ID
19910009839
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Barney, Richard D.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1990
Publication Information
Publication: 16th Space Simulation Conference Confirming Spaceworthiness Into the Next Millennium
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
91N19152
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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