タイトル | Variable Cycle Engine Technology Program Planning and Definition Study |
本文(外部サイト) | http://hdl.handle.net/2060/19790014913 |
著者(英) | Westmoreland, J. S.; Stern, A. M. |
著者所属(英) | Pratt and Whitney Aircraft Group |
発行日 | 1978-09-01 |
言語 | eng |
内容記述 | The variable stream control engine, VSCE-502B, was selected as the base engine, with the inverted flow engine concept selected as a backup. Critical component technologies were identified, and technology programs were formulated. Several engine configurations were defined on a preliminary basis to serve as demonstration vehicles for the various technologies. The different configurations present compromises in cost, technical risk, and technology return. Plans for possible variably cycle engine technology programs were formulated by synthesizing the technology requirements with the different demonstrator configurations. |
NASA分類 | AIRCRAFT PROPULSION AND POWER |
レポートNO | 79N23084 PWA-5581-12 NASA-CR-159539 |
権利 | No Copyright |