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Proceedings Paper

Experience With Supercritical Helium Cooling On A Rocket Sensor
Author(s): Donald P. Saletnik; Jens Peter Dybwad
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Paper Abstract

A large telescoped infrared sensor was successfully flown on a rocket. A supercritical helium cryogenic system was used to cool the various parts of the sensor and to avoid cooling problems associated with liquid/gas phase mixing during the weightless part of the flight. The design and operational experience are presented. Since the flight of the sen-sor lasted only eight minutes, most of the operational time was spent calibrating and testing the sensor on the ground. This testing was relatively expensive since approxi-mately 20,000 liters of liquid helium were consumed. Alternate approaches to the design and operations are discussed which can improve the economy of the calibration and testing operations.

Paper Details

Date Published: 10 November 1987
PDF: 4 pages
Proc. SPIE 0819, Infrared Technology XIII, (10 November 1987); doi: 10.1117/12.941834
Show Author Affiliations
Donald P. Saletnik, Utah State University (United States)
Jens Peter Dybwad, Utah State University (United States)

Published in SPIE Proceedings Vol. 0819:
Infrared Technology XIII
Irving J. Spiro, Editor(s)

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