| タイトル | Solid rocket booster thermal radiation model, volume 1 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19760017262 |
| 著者（英） | Watson, G. H.; Lee, A. L. |
| 著者所属（英） | Lockheed Missiles and Space Co. |
| 発行日 | 1976-03-01 |
| 言語 | eng |
| 内容記述 | A solid rocket booster (SRB) thermal radiation model, capable of defining the influence of the plume flowfield structure on the magnitude and distribution of thermal radiation leaving the plume, was prepared and documented. Radiant heating rates may be calculated for a single SRB plume or for the dual SRB plumes astride the space shuttle. The plumes may be gimbaled in the yaw and pitch planes. Space shuttle surface geometries are simulated with combinations of quadric surfaces. The effect of surface shading is included. The computer program also has the capability to calculate view factors between the SRB plumes and space shuttle surfaces as well as surface-to-surface view factors. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 76N24350
LMSC-HREC-TR-D496763-VOL-1
NASA-CR-144300 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/185754 |
