COMET Service Module thermal control system design using a Capillary Pumped Loop

Details COMET Service Module thermal control system design using a Capillary Pumped Loop COMET Service Module thermal control system design using a Capillary Pumped Loop

Jul 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992saei.confu....r&link_type=abstract

SAE, International Conference on Environmental Systems, 22nd, Seattle, WA, July 13-16, 1992, 12 p.

Physics

Pumps, Service Modules, Systems Analysis, Temperature Control, Heat Transfer, Microgravity, Requirements, Spacecraft Design

Scientific paper

The Commercial Experiment Transporter (COMET) Service Module thermal control system design based on a Capillary Pumped Loop (CPL) is presented. COMET aimed at performing experiments in the microgravity of space and returning one of two modules back to earth provides basic utilities, a tightly controlled thermal environment, attitude control, data management and communications. COMET is a two part Free Flyer based on a service module and a recovery system. The recovery sytem returns to earth by parachute after thirty days in orbit. The service module continues in orbit for up to two years.

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