21 January 1993 CIRRIS 1A cryogenic system performance
Author Affiliations +
The Cryogenic InfraRed Radiance Instrumentation for Shuttle (CIRRIS 1A) instrument, successfully flown and operated on the Shuttle Discovery from 28 April to 6 May 1991, was designed to operate at supercritical helium temperatures. During flight, the focal plane temperature control and telescope contamination purge systems performed as designed and 36 hours of excellent data was obtained; however, the parasitic helium flow rate was higher than expected. This paper reviews thermal data obtained for the CIRRIS 1A cooling system during both ground and flight operations. The temperature control and purge systems are discussed, along with helium flow rates, dewar helium pressure, and thermal stratification. In addition, possible reasons for the high on-orbit parasitic flow rate are presented.
© (1993) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Edward W. Vendell, Edward W. Vendell, David E. Morse, David E. Morse, Andrew Landoch, Andrew Landoch, } "CIRRIS 1A cryogenic system performance", Proc. SPIE 1765, Cryogenic Optical Systems and Instruments V, (21 January 1993); doi: 10.1117/12.140887; https://doi.org/10.1117/12.140887


Performance of the Spirit III cryogenic system
Proceedings of SPIE (October 22 1997)
Concepts For On-Orbit Servicing Of SIRTF
Proceedings of SPIE (July 17 1986)
Development of the SPIRIT III sensor
Proceedings of SPIE (January 20 1993)
Cold interferometric nulling demonstration in space (CINDIS)
Proceedings of SPIE (November 18 2003)

Back to Top