Thermal state of irregular spacecraft components

Details Thermal state of irregular spacecraft components Thermal state of irregular spacecraft components

Sep 1985

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1985kosis..23..719n&link_type=abstract

(Kosmicheskie Issledovaniia, vol. 23, Sept.-Oct. 1985, p. 719-728) Cosmic Research (ISSN 0010-9525), vol. 23, no. 5, March 1986,

Computer Science

Convective Heat Transfer, Heat Exchangers, Radiative Heat Transfer, Spacecraft Components, Spacecraft Temperature, Temperature Control, Cylindrical Shells, Spacecraft Structures, Spherical Shells

Scientific paper

Since the functional efficiency and reliability of spacecraft significantly depend on the conditions of internal and external heat exchange, it was decided to determine the conditions of heat exchange by the thermal state of the component, imposing specific thermal regulation requirements on the system. Analytical solutions are obtained for linearized problems of radiative-convective heat exchange for single-layer spherical shells, for two-layer spherical shells, for finite two-layer cylindrical shells, and for finite two-layer plates. The temperature of the surrounding medium is considered to be constant and to depend on position and time.

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