Performance Tests of the Fuel Pump for a Turbopump

터보펌프용 연료펌프의 성능 시험

  • 김대진 (한국항공우주연구원 터보펌프개발그룹) ;
  • 홍순삼 (한국항공우주연구원 터보펌프개발그룹) ;
  • 최창호 (한국항공우주연구원 터보펌프개발그룹) ;
  • 김진한 (한국항공우주연구원 터보펌프개발그룹)
  • Published : 2004.12.01

Abstract

Performance tests of the fuel pump for a turbopump unit have been successfully carried out in water environment. The tests are performed to evaluate the hydraulic and cavitation performances. The head and volute pressure distribution of the fuel pump followed the conventional similarity rule - unlike this, the secondary passage pressure distribution showed a small deviation from the conventional similarity rule. Also, critical cavitation number decreased as the rotational speed of the pump increased.

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