• Title/Summary/Keyword: 한국형우주발사체

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A Study On The Configuration Of UHD High Speed Digital Camera System In the Naro Space Center (나로우주센터 초고화질(UHD) 고속 디지털카메라 시스템에 대한 구성방안 연구)

  • Park, Doo-Jin;Noh, Young-Hwan
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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    • 2017.10a
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    • pp.536-538
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    • 2017
  • UHD high speed digital camera system will be installed around launch pad and launch complex tower to acquire high speed image for motion analysis of integral parts of launch vehicle during the lift-off of KSLV-II in the Naro space center. In this paper, We compared configuration of high speed digital camera system operating in the Naro space center with UHD high speed digital camera system for mission of KSLV-II.

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Design and Development of High Altitude Test Facility for Kick Motor (고공환경모사 시험설비 설계/개발)

  • Ryu, Jung-Hun;Lee, Jun-Ho;Suh, Hyuk;Jang, Ki-Won;Kim, Yong-Wook;Oh, Seung-Hyub
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2008.11a
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    • pp.403-404
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    • 2008
  • The 2nd stage Kick Motor under the national aerospace middle and long term plan operates over the height of 300Km. Rocket Motors, designed for operation in high altitude, need nozzles with large expansion ratio to improve thrust efficiency. Hence, to evaluate the performance of such rocket motors on the ground, similar low pressure with the operating condition has to be made for the ground test to prevent flow separation in the nozzle. This study is for the installation of the high altitude test facility and test result for Kick Motor.

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Development of the KSLV-I KM Case Manufacturing Process (KSLV-I KM 연소관 제작 공정 개발)

  • Kim, Joong-Suk;Lee, Won-Bok;Cho, In-Hyun;Kil, Gyoung-Sub
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2007.04a
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    • pp.193-196
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    • 2007
  • The motor case for the KSLV-I KM is the first satellite launch vehicle ever to be developed by Korea to deliver the 100 kg class satellite into Earth's low orbit. This SLV is made of two stages, and the 2nd stage is made of solid rocket motor. The motor case of the KM is made of all composite materials except for the interface structures. Manufacturing process for the motor case such as insulation, filament winding for the motor case, fabrications for the interface structures will be discussed in this paper.

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