High Intensity Acoustic Test for KOMPSAT-2 STM

다목적 실용위성 2호 구조-열모델의 음향 환경 시험

  • 김홍배 (한국항공우주연구원 우주시험연구그룹) ;
  • 문상무 (한국항공우주연구원 우주시험연구그) ;
  • 김영기 (한국항공우주연구원 우주시험연구그) ;
  • 우성현 (한국항공우주연구원 우주시험연구그) ;
  • 이상설 (한국항공우주연구원 우주시험연구그) ;
  • 김성훈 (한국항공우주연구원 위성본체연구그룹)
  • Published : 2002.05.01

Abstract

High intensity vibro-acoustic testing is the appropriate method for flight qualification testing of space flight vehicle which must ensure the acoustic environment of launch. To qualify vibro-acoustic environment during its flight, High Intensity Acoustic Test was performed for KOMPSAT-2(Korea Multi-Purpose SATellite) STM(Structural Thermal Model). This paper presents the detailed description on the high intensity acoustic test for KOMPSAT-2. Additionally the test results was compared with the analysis ones, which were estimated with 3-D SEA(Statistical Energy Analysis) model.

Keywords