| タイトル | Spacecraft control section for the improved Small Astronomy Satellite (SAS) |
| 本文（外部サイト） | http://hdl.handle.net/2060/19740007432 |
| 著者（英） | Townsend, M. R. |
| 著者所属（英） | NASA Goddard Space Flight Center |
| 発行日 | 1974-01-01 |
| 言語 | eng |
| 内容記述 | The upgraded spacecraft control section for the Small Astronomy Satellite is able to point its thrust axis to any direction in space; it can also spin or slow its outer body rotation to zero for star-locked pointing of side viewing experiments. A programmable telemetry system and delayed command system enhance the inherent capability of a spacecraft designed to be used for a variety of experiments, each of which can be built independently and attached just prior to final acceptance testing and launch. The design of this new spacecraft, whose first launch is scheduled for 1975, is provided in sufficient detail to permit the reader to ascertain its suitability for specific experiments. A summary of the spacecraft characteristics, project reliability requirements, and environmental test conditions are included in the appendices. |
| NASA分類 | SPACE VEHICLES |
| レポートNO | 74N15545
X-405-74-7
NASA-TM-X-70569 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/196083 |
