PASSIVE THERMAL CONTROL SYSTEMS FOR SPACE INSTRUMENTSMAKING – SCIENTIFIC BACKGROUND, QUALIFICATION, EXPLOITATION INSPACE
2009
Passive thermal control systems (TCS) are one of obligatory system of any space
mission, used as on large spacecraft and microsatellites Supporting of required temperature
range for space instruments is supported by rational design of TCS with optimal choice of
main thermal control components such as multilayer insulation, optical coatings, heat
conductive elements, heat insulation supports, thermal conductive gaskets, radiating surfaces
and other elements. New ideology in TCS design has come after appearance of new element
– heat pipe(s) which is a super heat conductive thermal conductor with constant or variable
thermal properties.
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