DocumentCode :
3053900
Title :
New application of reconnection electromagnetic launch (RCEML) with plate projectile: space application
Author :
Liyi, Li ; Xiaopeng, Li ; Yusheng, Hu
Author_Institution :
Harbin Inst. of Technol., China
fYear :
2003
fDate :
20-22 Nov. 2003
Firstpage :
427
Lastpage :
431
Abstract :
The paper presents a new application of RCEML with a plate projectile. Two kinds of projects are presented according to the load. The first project, for a large load, adopts electromagnetic assisted propulsion where the electromagnetic propulsion replaces the first stage rocket. When the projectile reaches a certain speed, another rocket stage will be needed to make it enter orbit. Based on the above technology, we designed a new electromagnetic assist system that has multilevel and multistage structure, and simulated the system. The electromagnetic propulsion completely replaces the rocket in the second stage. The paper shows that small loads including mini-satellites enter orbit directly at a certain speed by using the RCEML technology.
Keywords :
aerospace propulsion; aerospace simulation; electromagnetic launchers; projectiles; rocket engines; RCEML technology; electromagnetic assist propulsion; mini-satellite; multilevel structure; multistage structure; orbit entry; plate projectile; reconnection electromagnetic launch; two-stage rocket; Coils; Electromagnetic launching; Equations; Inductance; Paper technology; Projectiles; RLC circuits; Rockets; Space technology; Switches;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Recent Advances in Space Technologies, 2003. RAST '03. International Conference on. Proceedings of
Conference_Location :
Istanbul, Turkey
Print_ISBN :
0-7803-8142-4
Type :
conf
DOI :
10.1109/RAST.2003.1303954
Filename :
1303954
Link To Document :
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