The Thermal Control Surfaces Experiment (TCSE) is the most complex system retrieved after long term space exposure. The TCSE is a microcosm of complex electro-optical payloads being developed and flown. The objective of the TCSE on the LDEF was to determine the effects of the near-Earth orbital environment and the LDEF induced environment on spacecraft thermal control surfaces. The TCSE was a comprehensive experiment that combined in-space measurements with extensive post-flight analyses of thermal control surfaces to determine the effects of exposure to the low Earth orbit space environment. The TCSE was the first space experiment to measure the optical properties of thermal control surfaces the way they are routinely measured in the lab. The performance of the TCSE flight system on the LDEF was excellent.
Thermal Control Surfaces Experiment Flight System Performance
1992
15 pages
Report
No indication
English
Unmanned Spacecraft , Manned Spacecraft , Control surfaces , Temperature control , Thermal protection , Aerospace environments , Long duration exposure facility , Radiation dosage , Complex systems , Earth orbits , Electro-optics , Flight characteristics , Optical properties , Payload integration , Spaceborne experiments , Spacecraft environments , TCSE experiment