DocumentCode
2338413
Title
Controls and monitoring engineering challenges in the design of the supercharged ejector scramjet (SESJ) engine for spaceliner class transports
Author
Escher, William J D
Author_Institution
Space Transportation Div., NASA Headquarters, Washington, DC, USA
Volume
6
fYear
1995
fDate
21-23 Jun 1995
Firstpage
3937
Abstract
Top level controls and monitoring aspects of an advanced propulsion system aimed at future Earth/low-orbit transportation service are described. The example selected, the Supercharged Ejector Scramjet (SESJ) engine is a leading member of the airbreathing/rocket combined-cycle family of engines, which go well beyond traditional all-rocket systems, in the pursuit of achieving greatly reduced transportation costs and increased operational flexibility
Keywords
aerospace control; aerospace engines; monitoring; Earth/low-orbit transportation service; SESJ; advanced propulsion system; airbreathing/rocket combined-cycle engines; control; monitoring; operational flexibility; spaceliner class transports; supercharged ejector scramjet engine design; Aerospace industry; Costs; Design engineering; Engines; Monitoring; NASA; Propulsion; Rockets; Space technology; Transportation;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, Proceedings of the 1995
Conference_Location
Seattle, WA
Print_ISBN
0-7803-2445-5
Type
conf
DOI
10.1109/ACC.1995.532671
Filename
532671
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