Paper
1 November 1990 SHOOT cryogenic components: testing and applicability to other flight programs
Michael J. DiPirro, Michael E. Schein, Robert F. Boyle, Orlando Figueroa, David A. Lindauer, Daniel C. McHugh, Peter J. Shirron
Author Affiliations +
Abstract
Cryogenic components and techniques for the superfluid helium on-orbit transfer (SHOOT) flight demonstration are described. Instrumentation for measuring liquid quantity, position, flow rate, temperature, and pressure has been developed using the data obtained from the IRAS, Cosmic Background Explorer, and Spacelab 2 helium dewars. Topics discussed include valves and burst disks, fluid management devices, structural/thermal components, instrumentation, and ground support equipment and performance test apparatus.
© (1990) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Michael J. DiPirro, Michael E. Schein, Robert F. Boyle, Orlando Figueroa, David A. Lindauer, Daniel C. McHugh, and Peter J. Shirron "SHOOT cryogenic components: testing and applicability to other flight programs", Proc. SPIE 1340, Cryogenic Optical Systems and Instruments IV, (1 November 1990); https://doi.org/10.1117/12.23053
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Cited by 12 scholarly publications.
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KEYWORDS
Liquids

Helium

Cryogenics

Temperature metrology

Optical cryogenics

Sensors

Cavitation

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