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Developing Trends of Spinning Process for Manufacturing Thrust Chamber of Launch Vehicle

발사체 연소기 제작에서 스피닝 공정 개발 동향

  • Lee, Keumoh (Combustion Chamber Team, Korea Aerospace Research Institute) ;
  • Ryu, Chulsung (Combustion Chamber Team, Korea Aerospace Research Institute) ;
  • Choi, Hwanseok (Combustion Chamber Team, Korea Aerospace Research Institute) ;
  • Heo, Seongchan (Combustion Chamber Team, Korea Aerospace Research Institute) ;
  • Kwak, Junyoung (Combustion Chamber Team, Korea Aerospace Research Institute) ;
  • Choi, Younho (Research & Development 1 Team, Doowon Heavy Industry)
  • Received : 2015.06.02
  • Accepted : 2015.09.29
  • Published : 2015.12.01

Abstract

Spinning process is generally used for manufacturing axisymmetrical, thin-walled thickness and hollow circular cross-section parts. Traditional spinning technology is classified to conventional spinning and power spinning(shear spinning and flow forming). Literature surveys of spinning application for regenerative cooling chamber and divergent nozzle of liquid propellent rocket thrust chamber have been conducted. Most spinning technology has been used mandel for manufacturing chamber and nozzle. Recently, hot spinning has been used much compared to traditional cold spinning.

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