The Thermal Control Subsystem engineers task is to maintain the temperature of all spacecraft components, subsystems, and the total flight system within specified limits for all flight modes from launch to end-of-mission. In some cases, specific stability and gradient temperature limits will be imposed on flight system elements. The Thermal Control Subsystem of "normal" flight systems, the mass, power, control, and sensing systems mass and power requirements are below 10% of the total flight system resources. In general the thermal control subsystem engineer is involved in all other flight subsystem designs.
Spacecraft Design Thermal Control Subsystem
Presentation at University of Michigan, Ann Arbor, Michigan, January 31, 2008 ; 2008 ; Ann Arbor, MI, United States
2008-01-31
Preprint
Keine Angabe
Englisch
Spacecraft Design Thermal Control Subsystem
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