SBIR/STTR Research Award

Low Heat-Leak YBCO Leads for Satellite-Borne ADR Magnets

Award identifier 1a8f04785872dab8637c8b1fb88c9777cc2626808ebd239d12fa666bc03a2458Awarding agency National Aeronautics and Space Administration

Award amount

$124,418

Program and phase

SBIR · Phase I

Award year

2012

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
HYPRES INC
Proposal award date
2012-02-13
Contract end date
2012-08-13
UEI
Z3BBX7KX4WU5
Solicitation number
Not reported
Topic code
S1.07

Research abstract

Future satellite missions carrying X-ray spectrometers will be cooled to milliKelvin temperatures by multi-stage Adiabatic Demagnetization Refrigerators (ADR), which, in turn will be precooled by closed-cycle cryocoolers. Each stage of the ADR will use a low temperature superconducting magnet, which will periodically be energized via high temperature superconducting (HTS) leads. The present design of leads contributes a large fraction of the total heat load on the cryogenics system and so we propose to fabricate Yttria Barium Copper Oxide (YBCO) lead assemblies with a predicted heat load of about one order of magnitude lower than the established design that uses brittle filaments supported on a glass-fiber tube. Our suggested approach is to fabricate inherently tough and flexible leads in the 2A to 10A range from commercially available YBCO tape rated to over 200A. The substrates of such tapes are tough, strong low thermal conductivity metals which can be cut longitudinally into thin strips approximately 300 micrometers in width using a precision dicing saw. In principle, leads of any length or width can be made this way and tailored to a variety of specifications. In the region of the thermal gradient, the protective silver coating is removed and replaced by a non-conducting encapsulant; the as-manufactured silver coating is left at the ends to make electrical joints. This is a process which should lend itself well to small-scale manufacture. The strength and toughness of the leads means that they can be incorporated into a loom supported by taught Kevlar threads, which is a very low heat-leak method used extensively in space cryogenics. We expect that the overall result of this project will be to reduce significantly the size, weight and power requirement of the satellite-borne cryosystem and at the same time produce a lighter more robust lead structure.

Technology keywords

Not reported

Other awards by this recipient

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Awards with the same topic code

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Research funding history

255 SBIR/STTR records share this UEI (1985–2025). Reported award amounts total $91,527,586. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, Department of Energy, National Aeronautics and Space Administration, National Science Foundation, Department of Health and Human Services, Department of Commerce

Agency intelligence

National Aeronautics and Space Administration

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