Estimation of thermal conduction loads for structural supports of cryogenic spacecraft assemblies

Cryogenics

Volumn 44, Issue 6-8, 2004, Pages 421-424

  Ross Jr , Ronald G ^a  

^a CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

Conductivity; Launch loads; Spacecraft cryogenic supports; Thermal conduction loads

Indexed keywords

ASSEMBLY; COMPUTATIONAL METHODS; ESTIMATION; LOADS (FORCES); SPACECRAFT; STRENGTH OF MATERIALS; STRESSES; THERMAL CONDUCTIVITY;

CONDUCTIVITY; LAUNCH LOADS; SPACECRAFT CRYOGENIC SUPPORTS; THERMAL CONDUCTION LOADS;

CRYOGENICS;

EID: 2942589188     PISSN: 00112275     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.cryogenics.2004.02.019     Document Type: Conference Paper

References (8)

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6. Cafferty T, Landsat Thematic Mapper cryogenic radiator design. Private Communication.
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