DocumentCode :
3125481
Title :
An assessment of the state of cryocooler technology for space applications
Author :
Glaister, D.S. ; Donabedian, M. ; Curran, D.G.T. ; Davis, T.
Author_Institution :
Ball Aerosp. & Technol. Corp., Boulder, CO, USA
Volume :
5
fYear :
1999
fDate :
1999
Firstpage :
367
Abstract :
A survey is made which identifies more than 30 long life coolers for space applications covering a wide variety of thermodynamic cycles and configuration types. These coolers range in capacities from a few milliwatts to over 10 W at temperatures from 10 K to over 120 K and include single and multi-stage designs. The primary objectives of this study were to provide a hardware summary and performance comparison for potential space cryocooler users and to serve as an aid to the Air Force in determining future cryocooler development. The study identifies several existing flight qualified coolers and at least 12 programs which are likely to provide flight qualified units for cooling in the range of 10 to 150 K before the turn of the century. The survey presents an overview and status of the maturity of the various cryocoolers and performance comparisons are made at 35 K, 60 K, and 100 K
Keywords :
Joule-Thomson effect; Stirling engines; cooling; focal planes; infrared detectors; low-temperature production; reviews; space vehicles; 10 to 120 K; IR detectors; Joule-Thomson cooler; Stirling cooler; configuration types; cryocooler technology; flight qualified coolers; focal planes; hardware summary; long life coolers; multi-stage designs; performance comparison; pulse tube; reverse Brayton; single-stage designs; space applications; space cryocooler; thermodynamic cycles; Cryogenics; Extraterrestrial measurements; Infrared imaging; Infrared spectra; Infrared surveillance; Laboratories; Missiles; Space cooling; Space technology; Thermal force;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 1999. Proceedings. 1999 IEEE
Conference_Location :
Snowmass at Aspen, CO
Print_ISBN :
0-7803-5425-7
Type :
conf
DOI :
10.1109/AERO.1999.790215
Filename :
790215
Link To Document :
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