| タイトル | Aeroassist flight experiment guidance Quiet Time |
| 本文（外部サイト） | http://hdl.handle.net/2060/19880011860 |
| 著者（英） | Suit, William T.; Striepe, Scott A. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1988-02-01 |
| 言語 | eng |
| 内容記述 | The science experiments for the Aeroassist Flight Experiment (AFE) will be greatly enhanced by taking measurements with no Reaction Control System (RCS) contamination just before perigee. Methods of modifying the AFE guidance to accomplish this are discussed. Several methods that could give up to 30 seconds of quiet time were investigated and the results of these guidance modifications shown. A 20 second quiet time is definitely possible and a 30 second quiet time may be possible if the guidance can be inactive past perigee. Some of the most significant being the criterion for determining if the mission is threatened. A limited follow-on test program is outlined. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 88N21244
NASA-TM-100556
NAS 1.26:100556 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/146670 |
