Current Development Status of Inter-Propellant Seal for a Turbopump

터보펌프용 Inter-Propellant Seal의 개발 현황

  • 곽현덕 (한국항공우주연구원 터보펌프개발그룹) ;
  • 전성민 (한국항공우주연구원 터보펌프개발그룹) ;
  • 김진한 (한국항공우주연구원 터보펌프개발그룹)
  • Published : 2004.11.01

Abstract

To avoid an unexpected explosion occurring from a mixture of LOx and fuel, Inter-Propellant Seal (IPS) is used in a Turbopump. This paper presents a brief theoretical backgrounds of IPS and also reports preliminary test results. Tests were performed up to 1.5 MPa and 20,000 rpm and leakage performance of IPS was evaluated. As a result it was verified that leakage flow rate of IPS satisfied its design requirement.

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