A liquid helium 2 cryostat for space utilization

Details A liquid helium 2 cryostat for space utilization A liquid helium 2 cryostat for space utilization

Feb 1979

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1979snia.rept......&link_type=abstract

Final Report Societe Nationale Industrielle Aerospatiale, Cannes (France). Div. Systemes Balistiques et Spatiaux.

Physics

Cryostats, Liquid Helium 2, Space Laboratories, Aerospace Engineering, Fabrication, Hardware, Satellite-Borne Instruments, Spaceborne Experiments, Spacelab Payloads, Superfluidity, User Requirements

Scientific paper

A program for the development of a liquid helium 2 cryostat suitable for use in a variety of spaceborne experiments and capable of withstanding the rigors of launch and recovery is presented. Several different designs are examined, their pros and cons listed, and a detailed description of the basic configuration chosen is given. The final design has the advantages of employing already existing technologies, of being easily reusable, and of being well adapted to user requirements as it can be integrated with various instruments (superconductor magnets, supercooled telescopes, etc.). Fabrication specifications are discussed in detail, including descriptions of auxiliary hardware (tanks, supports, valves, tubing).

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