DocumentCode :
1973212
Title :
Dynamic simulation and anlysis of rocket electromagnetic launcher
Author :
Wang, Kang ; Xiang, Hongjun ; Li, Zhiyuan
Author_Institution :
Dept. of Ammunition Eng., Shijiazhuang Mech. Eng. Coll., Shijiazhuang, China
fYear :
2011
fDate :
16-18 Sept. 2011
Firstpage :
3014
Lastpage :
3016
Abstract :
Current rocket launching may cause high temperature, high pressure and many poisonous gases, which is harmful for the instruments and operators in the launching site. It introduces a new technology of cold emission for the rocket launching based on the technology of electromagnetic inductive launching. It introduces the principle of the system and builds the mathematical model for electromagnetic launcher. And then it simulates the rocket electromagnetic launching system by Ansoft and validates the feasibility of the system.
Keywords :
electromagnetic launchers; mathematical analysis; rockets; Ansoft; electromagnetic inductive launching; launching site; mathematical model; poisonous gas; rocket electromagnetic launcher analysis; Defense industry; Electromagnetics; Mathematical model; Military aircraft; Missiles; Plasmas; Rockets; ansoft; electromagnetic launch; rocket; simulation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electrical and Control Engineering (ICECE), 2011 International Conference on
Conference_Location :
Yichang
Print_ISBN :
978-1-4244-8162-0
Type :
conf
DOI :
10.1109/ICECENG.2011.6057043
Filename :
6057043
Link To Document :
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