| タイトル | The effects of solid rocket motor effluents on selected surfaces and solid particle size, distribution, and composition for simulated shuttle booster separation motors |
| 本文（外部サイト） | http://hdl.handle.net/2060/19760009081 |
| 著者（英） | Trenkle, J. J.; Linton, R. C.; Jex, D. W.; Wilkes, D. R.; Russell, W. M. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 1976-01-12 |
| 言語 | eng |
| 内容記述 | A series of three tests was conducted using solid rocket propellants to determine the effects a solid rocket plume would have on thermal protective surfaces (TPS). The surfaces tested were those which are baselined for the shuttle vehicle. The propellants used were to simulate the separation solid rocket motors (SSRM) that separate the solid rocket boosters (SRB) from the shuttle launch vehicle. Data cover: (1) the optical effects of the plume environment on spacecraft related surfaces, and (2) the solid particle size, distribution, and composition at TPS sample locations. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 76N16169
NASA-TM-X-64975 |
| 権利 | No Copyright |
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