Acoustic Loads Test of the Upper Stage of KSLV-I

소형위성발사체 상단부의 음향하중시험

  • 전영두 (한국항공우주연구원 우주발사체사업단) ;
  • 박종찬 (한국항공우주연구원, 우주발사체사업단) ;
  • 정의승 (한국항공우주연구원, 우주발사체사업단) ;
  • 박정주 (한국항공우주연구원, 우주발사체사업단) ;
  • 조광래 (한국항공우주연구원, 우주발사체사업단)
  • Published : 2007.05.10

Abstract

This paper introduces the results of acoustic loads test conducted on the upper stage assembly of KSLV-I, which is the first Korea space launch vehicle. A launch vehicle and its payloads are subjected to severe acoustic pressure loading when they lift off and ascent during the transonic periods. Acoustic loadings are spreaded out broad frequncy-spectrum up to 10,000Hz. Acoustic loads are a primary source of structural random vibration of the upper stage and payloads. Therefore, in order to verify the structural integrity of the upper stage assembly of KSLV-I and the survivability of its components under severe random vibration environment, acoustic loads test is conducted in the high intensity acoustic chamber with 142dB (overall SPL). The results show the structural design and component random vibration specifications well meet with the environmental requirements.

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