| タイトル | Capillary acquisition devices for high-performance vehicles: Executive summary |
| 本文（外部サイト） | http://hdl.handle.net/2060/19800010908 |
| 著者（英） | Bradshaw, R. D.; Blatt, M. H.; Risberg, J. A. |
| 著者所属（英） | General Dynamics/Convair |
| 発行日 | 1980-02-01 |
| 言語 | eng |
| 内容記述 | Technology areas critical to the development of cryogenic capillary devices were studied. Passive cooling of capillary devices was investigated with an analytical and experimental study of wicking flow. Capillary device refilling with settled fluid was studied using an analytical and experimental program that resulted in successful correlation of a versatile computer program with test data. The program was used to predict Centaur D-1S LO2 and LH2 start basket refilling. Comparisons were made between the baseline Centaur D-1S propellant feed system and feed system alternatives including systems using capillary devices. The preferred concepts from the Centaur D-1S study were examined for APOTV and POTV vehicles for delivery and round trip transfer of payloads between LEO and GEO. Mission profiles were determined to provide propellant usage timelines and the payload partials were defined. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 80N19185
GDC-CRAD-80-003
NASA-CR-159658 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/173138 |
