| タイトル | System concept for the pinhole/occulter facility payload |
| 著者（英） | Howell, J. T.; Dabbs, J. R.; Srinivas, R. |
| 著者所属（英） | NASA Marshall Space Flight Center; Teledyne Brown Engineering |
| 発行日 | 1986-10-01 |
| 言語 | eng |
| 内容記述 | The results of a study of the systems concept of the Pinhole/Occulter Facility (PDF) to fly on the Shuttle as a Spacelab payload are reported. In particular, attention is given to the POF configuration and structural/mechanical concepts; POF payload structural concept development; POF payload new baseline configuration; POF pointing requirements and the Spacelab Instrument Pointing System capabilities and limitations; and pointing control implementation approach. The discussion also covers POF command and data management system configuration; POF processor software assessment; and thermal design concept. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 87A15804
IAF PAPER 86-05 |
| 権利 | Copyright |
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