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NASA NTRS · 20060040792

Development of a Thermal Isolation Structure for Aerospace Cryogenic Instruments

Abstract

A proof of concept prototype cryostat has been developed to demonstrate the ability to accommodate low temperature science investigations within the constraints of the Hitchhiker siderail carrier on the space shuttle.

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BibTeXRIS

Nash, A., Robeck, L.. 1999-07-01. Development of a Thermal Isolation Structure for Aerospace Cryogenic Instruments. https://ntrs.nasa.gov/citations/20060040792

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