| タイトル | Parallel-burn options for dual-fuel single-stage orbital transports |
| 著者（英） | Martin, J. A. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1978-02-01 |
| 言語 | eng |
| 内容記述 | A parallel-burn version of a single-stage vehicle for transport from the earth to low-earth orbit using two fuels and rocket propulsion is considered. New engine results were incorporated in vehicle performance and design studies. The results indicate that a hydrogen-cooled gas generator cycle engine provides attractive vehicle performance and that there is little incentive for increasing the chamber pressure beyond 27 MPa. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 78A22201 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/433972 |
