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