| タイトル | Technology requirements for advanced earth-orbital transportation systems |
| 本文（外部サイト） | http://hdl.handle.net/2060/19780003243 |
| 著者（英） | Haefeli, R. C.; Winter, M. G.; Littler, E. G.; Hurley, J. B. |
| 著者所属（英） | Martin Marietta Corp. |
| 発行日 | 1977-10-01 |
| 言語 | eng |
| 内容記述 | Areas of advanced technology that are either critical or offer significant benefits to the development of future Earth-orbit transportation systems were identified. Technology assessment was based on the application of these technologies to fully reusable, single-stage-to-orbit (SSTO) vehicle concepts with horizontal landing capability. Study guidelines included mission requirements similar to space shuttle, an operational capability begining in 1995, and main propulsion to be advanced hydrogen-fueled rocket engines. Also evaluated was the technical and economic feasibility of this class of SSTO concepts and the comparative features of three operational take-off modes, which were vertical boost, horizontal sled launch, and horizontal take-off with subsequent inflight fueling. Projections of both normal and accelerated technology growth were made. Figures of merit were derived to provide relative rankings of technology areas. The influence of selected accelerated areas on vehicle design and program costs was analyzed by developing near-optimum point designs. |
| NASA分類 | SPACE TRANSPORTATION |
| レポートNO | 78N11186
NASA-CR-2866 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/180694 |
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