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LDR cryogenicsA brief summary from the 1985 Large Deployable Reflector (LDR) Asilomar 2 workshop of the requirements for LDR cryogenic cooling is presented. The heat rates are simply the sum of the individual heat rates from the instruments. Consideration of duty cycle will have a dramatic effect on cooling requirements. There are many possible combinations of cooling techniques for each of the three temperatures zones. It is clear that much further system study is needed to determine what type of cooling system is required (He-2, hybrid or mechanical) and what size and power is required. As the instruments, along with their duty cycles and heat rates, become better defined it will be possible to better determine the optimum cooling systems.
Document ID
19900004156
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nast, T.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Date Acquired
September 6, 2013
Publication Date
August 15, 1988
Publication Information
Publication: Jet Propulsion Lab., California Inst. of Tech., Report of the Asilomar 3 LDR Workshop
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
90N13472
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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