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Experimental design for the evaluation of high-T(sub c) superconductive thermal bridges in a sensor satelliteInfrared sensor satellites, which consist of cryogenic infrared sensor detectors, electrical instrumentation, and data acquisition systems, are used to monitor the conditions of the earth's upper atmosphere in order to evaluate its present and future changes. Currently, the electrical connections (instrumentation), which act as thermal bridges between the cryogenic infrared sensor and the significantly warmer data acquisition unit of the sensor satellite system, constitute a significant portion of the heat load on the cryogen. As a part of extending the mission life of the sensor satellite system, the researchers at the National Aeronautics and Space Administration's Langley Research Center (NASA-LaRC) are evaluating the effectiveness of replacing the currently used manganin wires with high-temperature superconductive (HTS) materials as the electrical connections (thermal bridges). In conjunction with the study being conducted at NASA-LaRC, the proposed research is to design a space experiment to determine the thermal savings on a cryogenic subsystem when manganin leads are replaced by HTS leads printed onto a substrate with a low thermal conductivity, and to determine the thermal conductivities of HTS materials. The experiment is designed to compare manganin wires with two different types of superconductors on substrates by determining the heat loss by the thermal bridges and providing temperature measurements for the estimation of thermal conductivity. A conductive mathematical model has been developed and used as a key tool in the design process and subsequent analysis.
Document ID
19950007693
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Scott, Elaine P.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Lee, Kasey M.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
September 6, 2013
Publication Date
October 10, 1994
Subject Category
Spacecraft Instrumentation
Report/Patent Number
NASA-CR-197003
NAS 1.26:197003
Report Number: NASA-CR-197003
Report Number: NAS 1.26:197003
Accession Number
95N14106
Funding Number(s)
CONTRACT_GRANT: NAG1-1500
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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