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
Link To Document :
بازگشت