| タイトル | PC-402 Pioneer Venus orbiter spacecraft mission operational characteristics document |
| 本文（外部サイト） | http://hdl.handle.net/2060/19820004217 |
| 著者（英） | Butterworth, L. W.; Tadler, G. A.; Drean, R. J.; Salvatore, J. O.; Fisher, J. N.; Filetti, K. A.; Porzucki, J.; Nowak, L. A.; Daniel, R. E.; Barker, F. C. |
| 著者所属（英） | Hughes Aircraft Co. |
| 発行日 | 1978-02-01 |
| 言語 | eng |
| 内容記述 | The operational characteristics of the Orbiter spacecraft and its subsystems are described. In extensive detail. Description of the nominal phases, system interfaces, and the capabilities and limitations of system level performance are included along with functional and operational descriptions at the subsystem and unit level the subtleties of nominal operation as well as detailed capabilities and limitations beyond nominal performance are discussed. A command and telemetry logic flow diagram for each subsystem is included. Each diagram encountered along each command signal path into, and each telemetry signal path out of the subsystem. Normal operating modes that correspond to the performance of specific functions at the time of specific events in the mission are also discussed. Principal backup means of performing the normal Orbiter operating modes are included. |
| NASA分類 | ASTRONAUTICS (GENERAL) |
| レポートNO | 82N12090
SCG-86112A
NASA-CR-166260 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/167594 |
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