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Development of space stable thermal control coatings for use on large space vehicles. [effects of ultraviolet radiation
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Harada, Y. Gilligan, J. E. |
| Copyright Year | 1974 |
| Description | The development of a large scale manufacturing method for the production of a stable zinc orthotitanate pigment is discussed. Major emphasis was placed on the evaluation of ultraviolet radiation stability tests of pigments derived from coprecipitated and individually precipitated oxalates. Emphasis was also placed on an investigation of the conditions (time and temperature) leading to high reflectance and high optical stability. Paints were formulated in OI-650 and in OI-650G vehicles from pigments which were prepared at various temperatures. Analyses of ultraviolet irradiation test data were conducted regarding optimum pigment preparation parameters and treatment conditions. |
| File Size | 2893517 |
| Page Count | 113 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750012379 |
| Archival Resource Key | ark:/13960/t4pk55b4b |
| Language | English |
| Publisher Date | 1974-10-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Stability Tests Spacecraft Shielding Ultraviolet Radiation Performance Tests Thermal Control Coatings Zinc Coatings Pigments Oxalates Protective Coatings Reflectance Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
