• 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