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Shuttle Infrared Telescope FacilityThe Shuttle Infrared Telescope Facility (SIRTF) will combine high sensitivity with the flexibility offered by the Space Transportation System. A recently completed study has generated a preliminary design which demonstrates the feasibility of SIRTF. The 1.0 to 1.5 meter aperture, f/8 Gregorian telescope will be cooled to 20 K by a stored supercritical helium system. The telescope will be pointed and stabilized at two levels: the European-developed Instrument Pointing System provides primary pointing and stabilization; and an internal star tracker senses residual errors and drives a folding mirror inside the telescope to null the errors. The folding mirror can also be driven by square or triangular waves to provide space chopping or small-area scanning.
Document ID
19770053163
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Mccarthy, S. G.
(Hughes Aircraft Co., Strategic Systems Div., Culver City Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1976
Subject Category
Astronomy
Meeting Information
Meeting: Seminar on Modern utilization of infrared technology II: Civilian and military
Location: San Diego, CA
Start Date: August 26, 1976
End Date: August 27, 1976
Accession Number
77A36015
Funding Number(s)
CONTRACT_GRANT: NAS2-8494
Distribution Limits
Public
Copyright
Other

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