• Title/Summary/Keyword: 2단 궤도 진입비행체

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Current Technological Trends in Hypersonic Flight with Air-Breathing Propulsion System (차세대 극초음속 공기흡입식 추진기관의 개발 동향)

  • Lee, Yang-Ji;Kang, Sang-Hun;Yang, Soo-Seok
    • Current Industrial and Technological Trends in Aerospace
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    • v.7 no.1
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    • pp.43-55
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    • 2009
  • Advanced countries in aerospace have been struggle to realize the hypersonic air-breathing system since originating the concept of the hypersonic air-breathing propulsion system during the first half of the twentieth century. At last, NASA's X-43A Hyper-X did successful Mach 10 flight in November 2004. Each countries are running the program to applicate this hypersonic air-breathing propulsion system to SSTO(Single Stage to Orbit) or TSTO(Two Stage to Orbit) vehicle or hypersonic missile system at present. In this paper, we wrote the history and current issues of the hypersonic air-breathing propulsion system and hypersonic flight with the hypersonic air-breathing propulsion system.

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Prediction of Kick Motor Mass Variation (킥모터 무게 변화 예측)

  • Kil, Gyoung-Sub;Kho, Hyeon-Seok;Kim, Byung-Hun;Cho, In-Hyun
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2008.11a
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    • pp.203-206
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    • 2008
  • Kick motor(KM) for KSLV-I second stage propulsion system is the main hardware that is necessary for launching satellite to it's track. The mass of the kick motor changes with combustion time because the heat insulator is ablated and propellant is used and slag is piled up. We predicted mass change with the flight time using ground combustion data of KM composed of case, propellant, nozzle, ignitor and slag. The mass prediction of kick motor can be used for calculating the two stage mass and center of gravity history.

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