Rocket propulsion device and method for assembling rocket propulsion device

作者： Soon Il Moon , Jae Beom Park , Bang Eop Lee , Sung Han Park

DOI:

关键词: Propellant 、 Line (electrical engineering) 、 Spacecraft propulsion 、 Nozzle 、 Tube (container) 、 Engineering 、 Aerospace engineering 、 Thrust

摘要: A rocket propulsion device including, a case having propellant therein, the in form of tube, nozzle at least part inserted case, and configured to discharge gas upon burning propellant, locking unit disposed be wound on nozzle, band both ends open, wherein through hole for inserting therein is formed one region circumference are located facing region, whereby simplified structure facilitated alignment thrust line can implemented.