| タイトル | STV engine requirements |
| 著者（英） | Huffaker, C. F.; Redus, J. R.; Kelley, D. L. |
| 著者所属（英） | Martin Marietta Corp.; NASA Marshall Space Flight Center |
| 発行日 | 1990-09-01 |
| 言語 | eng |
| 内容記述 | The Space Exploration Initiative program and the Space Transfer Vehicle studies provide the opportunity to evaluate the engine requirements for the next generation space engine within the context of a credible but technologically demanding program. Some of these requirements are generic, basically independent of the architecture, and others are mission and configuration dependent. Generic requirements include high reliability, space-basing, man-rataing, long life and reusability, and extended health monitoring, including automatic pre-mission checkout. Mission and configuration dependent requirements include vehicle/engine interfaces, engine throttling, performance specifications, engine system architecture, and operational requirements. It is argued that engine technology requirements must be extended from the usual performance-related issues to encompass reliability, space-basing, life, and extended health monitoring. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 91A10106
AIAA PAPER 90-3707 |
| 権利 | Copyright |
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