Many requirements must be satisfied in order to achieve a successful spacecraft mission. One very pervasive requirement is that every spacecraft component must be maintained within either operating or survival temperature limits at all times. This is a very difficult requirement to satisfy because of the many boundary conditions.
Hemispherical Thermal Emittance of Copper as a Function of Oxidation Conditions
1971-01-01
21 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Measurement of Total Hemispherical Emittance on Spacecraft Thermal Control Coatings
SAE Technical Papers | 1992
|