Large Space Telescope support systems module thermal control

Details Large Space Telescope support systems module thermal control Large Space Telescope support systems module thermal control

May 1975

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1975thph.confq....c&link_type=abstract

American Institute of Aeronautics and Astronautics, Thermophysics Conference, 10th, Denver, Colo., May 27-29, 1975, 9 p.

Physics

Computerized Simulation, Hubble Space Telescope, Spacecraft Modules, Support Systems, Temperature Control, Mathematical Models, Satellite Design, Systems Engineering

Scientific paper

In 1982, an unmanned three-meter class Cassegrainian telescopic system referred to as the Large Space Telescope (LST) will be placed in earth orbit by the Shuttle. The LST consists of a telescope system and surrounding support structure that is referred to as the support system module (SSM). This paper summarizes the thermal control subsystem for several candidate SSM designs. Major emphasis has been given to the LST/SSM design concept that includes a thermally isolated aft cylinder compartment that contains subsystem components. Requirements, interfaces and thermal math modeling methods are presented. Analysis results demonstrate that a cold-biased thermal design using electrical heaters is promising.

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