Space environment simulation to test satellite thermal control coatings. Volume 2: Annex 1
Abstract
Optical properties measured in situ at -35C and at various exposure stages up to one year are tabulated for thermal control coatings tested during space environment simulation. Results show: (1) spectral reflectance for 13 wavelengths; (2) variation with respect to the initial measurement, i.e., before irradiation and deposition; (3) solar reflectance including ultraviolet, visible, and infrared radiation, as well as the total spectrum (295 to 4,000 nm); (4) variations of solar reflectance with respect to initial values; (5) solar absorptance (calculated as a complement at 1.00 of solar reflectance in the same wavelength domain); and (6) variations of these solar reflectances with respect to initial values.
- Publication:
-
Space environment simulation to test satellite thermal control coatings. Volume 2: Annex 1 ESA
- Pub Date:
- 1983
- Bibcode:
- 1983sest....2Q.....
- Keywords:
-
- Optical Reflection;
- Satellite Temperature;
- Space Environment Simulation;
- Spacecraft Contamination;
- Thermal Control Coatings;
- Electron Irradiation;
- Ots (Esa);
- Proton Irradiation;
- Synchronous Satellites;
- Tables (Data);
- Thermal Simulation;
- Ultraviolet Radiation;
- Vacuum Chambers;
- Launch Vehicles and Space Vehicles