Reduced Actuator Set for Pressure Control and Thrust Distribution for Multinozzle Propulsion Systems
Joint Authors
Bang, Hyochoong
Lim, Yeerang
Lee, Jaecheong
Huh, Hwanil
Lee, Hosung
Source
International Journal of Aerospace Engineering
Issue
Vol. 2017, Issue 2017 (31 Dec. 2017), pp.1-11, 11 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2017-05-08
Country of Publication
Egypt
No. of Pages
11
Abstract EN
This study investigated an approach to reduce the number of actuators used for internal pressure control and thruster allocation in a multinozzle solid propulsion system.
In the proposed design, the throat areas of four divert nozzles are controlled by only three actuators, and chamber pressure maintenance and thrust distribution are achieved by controlling the throat areas.
Using the proposed actuator set, thrust allocation can be accomplished in a more efficient way than when independent actuators are employed for each nozzle.
American Psychological Association (APA)
Lim, Yeerang& Lee, Jaecheong& Bang, Hyochoong& Huh, Hwanil& Lee, Hosung. 2017. Reduced Actuator Set for Pressure Control and Thrust Distribution for Multinozzle Propulsion Systems. International Journal of Aerospace Engineering،Vol. 2017, no. 2017, pp.1-11.
https://search.emarefa.net/detail/BIM-1158017
Modern Language Association (MLA)
Lim, Yeerang…[et al.]. Reduced Actuator Set for Pressure Control and Thrust Distribution for Multinozzle Propulsion Systems. International Journal of Aerospace Engineering No. 2017 (2017), pp.1-11.
https://search.emarefa.net/detail/BIM-1158017
American Medical Association (AMA)
Lim, Yeerang& Lee, Jaecheong& Bang, Hyochoong& Huh, Hwanil& Lee, Hosung. Reduced Actuator Set for Pressure Control and Thrust Distribution for Multinozzle Propulsion Systems. International Journal of Aerospace Engineering. 2017. Vol. 2017, no. 2017, pp.1-11.
https://search.emarefa.net/detail/BIM-1158017
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1158017