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Long life feasibility study for SIRTFThe Phase A baseline for the Shuttle Infrared Telescope Facility (SIRTF) consists of an 85-cm diameter Cassegrain telescope, cooled to temperatures in the range from 10 to 20 K to provide background limited imaging for up to six instruments contained within a multiple instrument chamber (MIC). Colder temperature zones are also provided. A cryogenics system for a 15-day mission lifetime was first considered. In another study, the feasibility was assessed to extend the lifetime of the baseline SIRTF concept to at least six months, taking into account a mission involving the use of a space platform or a free-flyer configuration. According to the considered requirements, the optics temperature is to be kept below 10 K for at least 30 days. The temperatures are not to exceed 20 K at the end of the six months mission. It is shown that by using solid hydrogen, long-life operation is feasible with present technology.
Document ID
19860030610
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Naes, L. G.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Nast, T. C.
(Lockheed Research Laboratories Palo Alto, CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
86A15348
Funding Number(s)
CONTRACT_GRANT: NAS2-11155
Distribution Limits
Public
Copyright
Other

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