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The Instrument Test Dewar (ITD): Testing satellite instruments at 1.5 KThe Instrument Test Dewar (ITD) is a cryogenic facility designed and built to test Cosmic Background Explorer (COBE) satellite instruments at 1.5 K. The facility provides a high vacuum and thermal environment with payload thermal, electrical and optical interfaces. There are two concentric vacuum spaces which are not hermitically sealed. The instrument vacuum space is 81.28 cm by 243.84 cm and is cooled by an LHe shroud. The guard vacuum space surrounds an LN2 shroud. There are two separate cryosorption pumping systems and a mechanical LHe pumping system. The data acquisition systems provide payload and housekeeping data. There have been various problems with the facility, and changes and improvements have been made to assure optimum test conditions. COBE instrument testing has been completed on structural, thermal model hardware and the protoflight units.
Document ID
19890003233
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Milam, Laura J.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1988
Publication Information
Publication: 15th Space Simulation Conference: Support t he Highway to Space Through Testing
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
89N12604
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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