| タイトル | Parachute design for Galileo Jupiter entry probe |
| 著者（英） | Rodier, R. W.; Thuss, R. C.; Terhune, J. E. |
| 著者所属（英） | NASA Ames Research Center|Pioneer Parachute Co., Inc.|General Electric Co. |
| 発行日 | 1981-10-01 |
| 言語 | eng |
| 内容記述 | This paper discusses the parachute subsystem used on an atmospheric entry probe that will descend through the clouds of Jupiter. The entry probe is a part of the Galileo Project to be launched in 1985 aboard the Space Shuttle; the entry probe will encounter the planet in 1988. The parachute subsystem consists of a pilot parachute and a main parachute, and both are of conventional conical ribbon design. Key considerations in the design of the parachutes and a summary of the parachute subsystem test program, which includes two air drop tests and a systems drop test (balloon launched), are presented. |
| NASA分類 | SPACE TRANSPORTATION |
| レポートNO | 82A10426
AIAA PAPER 81-1951 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/413506 |
