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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NO79N23084
PWA-5581-12
NASA-CR-159539
権利No Copyright


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