The SHOOT cryogenic components - Testing and applicability to other flight programs

Details The SHOOT cryogenic components - Testing and applicability to other flight programs The SHOOT cryogenic components - Testing and applicability to other flight programs

Nov 1990

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1990spie.1340..291d&link_type=abstract

IN: Cryogenic optical systems and instruments IV; Proceedings of the Meeting, San Diego, CA, July 10-12, 1990 (A92-22851 08-31).

Computer Science

Performance

Cryogenic Equipment, Liquid Helium, Orbit Transfer Vehicles, Orbital Servicing, Superfluidity, Cryogenic Fluid Storage, Cryopumping, Flight Tests, Orbital Lifetime, Thermosiphons

Scientific paper

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.

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