The potential of zinc orthotitanate as a pigment for spacecraft thermal control was demonstrated. The properties and performance of pigments prepared by solid state, coprecipitation, and mixed oxalate methods were compared. Environmental tests and subsequent spectral analysis were given primary emphasis.
Development of Space-Stable Thermal Control Coatings for Use on Large Space Vehicles
1976
466 pages
Report
No indication
English
Coatings, Colorants, & Finishes , Physical & Theoretical Chemistry , Unmanned Spacecraft , Spacecraft shielding , Thermal control coatings , Pigments , Aerospace environments , Chemical reactions , Electron paramagnetic resonance , Environmental tests , Stoichiometry , Titanates , Zinc compounds , Zinc titanates , Synthesis(Chemistry)