| タイトル | Apollo experience report guidance and control systems: Lunar module abort guidance system |
| 本文（外部サイト） | http://hdl.handle.net/2060/19750018954 |
| 著者（英） | Kurten, P. M. |
| 著者所属（英） | NASA Johnson Space Center |
| 発行日 | 1975-07-01 |
| 言語 | eng |
| 内容記述 | The history of a unique development program that produced an operational fixed guidance system of inertial quality is presented. Each phase of development, beginning with requirement definition and concluding with qualification and testing, is addressed, and developmental problems are emphasized. Software generation and mission operations are described, and specifications for the inertial reference unit are included, as are flight performance results. Significant program observations are noted. |
| NASA分類 | ASTRONAUTICS (GENERAL) |
| レポートNO | 75N27026
JSC-S-424
NASA-TN-D-7990 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/189485 |
