| タイトル | Silica RSI for Application to the Shuttle Orbiter |
| 著者（英） | Jue, J.; Forsberg, K. J.; Kural, M. H.; Velligan, F. A. |
| 著者所属（英） | Lockheed Missiles and Space Co. |
| 発行日 | 1973-09-01 |
| 言語 | eng |
| 内容記述 | Silica reusable surface insulation is analyzed for its cold soak properties, bond properties at low temperature, gap and step heating effects, and aerodynamic surface roughness effects to determine space shuttle weight and cost sensitivity to structure subsystem weights. Computerized simulation studies show that total program cost savings of silica (vs. mullite) exceed thermal protection system design and development costs and that an early introduction of silica increases total program cost savings. |
| NASA分類 | MATERIALS, NONMETALLIC |
| レポートNO | 73N33496 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/68381 |
|
