• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.1184-1187
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• 2017

The space launch vehicle needs the verification of each stage's propulsion system. The Propulsion System Test Complex(PSTC) is constructed for developing KSLV-II in the Naro space center. Hydraulic and pneumatic system of PSTC should supply propellants and various gases to propulsion system module according to required condition. This paper introduces liquid oxygen filling system of PSTC.

• Defense and Technology
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• no.9 s.163
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• pp.32-37
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• 1992

선진국의 유도탄 고체 추진기관의 연구 개발 동향 파악은 우리의 유도탄 추진기관 연구개발의 좌표확인과 나아갈 방향을 설정하는데 대단히 중요합니다. 이 글에서는 유도탄에 사용되는 고체 추진기관에 대한 세계적 연구 동향을 분석하였습니다 연구 동향은 추진시스템과 추진기관 부시스템 및 부품 2가지 부분으로 나누어 살펴보았습니다. 추진시스템은 기존의 로켓과는 다른 닥티드로켓/램젯, 펄스 모타등의 새로운 추진시스템의 연구동향을 분석하였으며, 기존 고체 로켓 모타부품의 연구개발 및 동향을 기술하였습니다

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2012.05a
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• pp.489-492
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• 2012

Basic design result for propulsion system test complex(PSTC) of KSLV-II is briefly described. KSLV-II is a three stage launch vehicle will be used liquid rocket engine for each. PSTC is will be used for development and performances qualification tests of $1^{st}/2^{nd}/3^{rd}$ propulsion systems for KSLV-II. In the future, this result will be applied to critical design and manufacturing of PSTC after deciding lay-out and operating program.

• The Bulletin of The Korean Astronomical Society
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• v.37 no.2
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• pp.153.2-153.2
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• 2012

발사체 추진기관은 추진제 및 각종 고압가스류를 엔진으로 공급하는 기능, 지상에서 추진제를 발사체로 충전/배출하는 기능, 저온 산화제를 냉각하기 위한 순환 기능, 추진제 탱크를 가압하는 기능, 지상에서 온보드 밸브를 구동하는 기능, 내부 공간 및 라인 퍼지 기능 등을 수행한다. 이와 같은 기능을 수행하기 위해 발사체에는 타 시스템과는 별도로 추진기관 원격제어 시스템을 구성한다. 제어 시스템은 크게 온보드 시퀀스 및 추진제 탱크 압력 제어, 추진제 및 고압가스 충전/배출 제어, 발사체 기능 확인, 내부 기밀 확인 및 발사 직전까지의 상태 모니터링을 위해 구성한 지상측정시스템(GMS), 비행 중 추진기관 상태를 모니터링하기 위한 텔레메트리시스템(TMS)으로 분류한다. 본 논문에서는 일반적인 발사체 추진기관 운용 및 제어 개념을 제어 기능, 시스템 구성, 작동 원리의 단계로 사례와 함께 제시하였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.1180-1183
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• 2017

The Propulsion System Test Complex (PSTC) is constructed for developing KSLV-II in the Naro space center. The KSLV-II uses LOX for oxidizer and oxidizer filling algorithm is developed for supplying oxidizer to KSLV-II. This paper introduces oxidizer filling algorithm.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2011.11a
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• pp.789-792
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• 2011

Before doing the flight test, the ground test for liquid rocket propulsion system is helpful for improving its reliability and reducing the development money. Therefore, by constructing the Propulsion System Test Complex for heavy liquid rocket propulsion system development, we expect that it will be the first step for making the commercial launcher which will be competitive in the international launch service market.

• Journal of the Korean Society of Propulsion Engineers
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• v.15 no.5
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• pp.89-95
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• 2011

Korea Space Launch Vehicle II (KSLV-II) planned to launch in 2021 is 3 stage rocket which can inject 1.5 ton satellite in low earth orbit. KSLV-II will adapt the newly developed liquid rocket engines for its propulsion system of each stage. For the evaluation of development level for rocket engine, integrated system test performed in appropriate facility is needed. In this study, test article and major parameters for certifying the propulsion system of KSLV-II were reviewed and optimum test cycle and test duration for satisfying system reliability requirement were illustrated.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2011.11a
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• pp.797-800
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• 2011

For the space launch vehicle, propulsion system is the most important subsystem among others. For the evaluation of development level for rocket engine, integrated system test performed in appropriate facility is needed. In this study, test article and major parameters for certifying the propulsion system of launch vehicle were reviewed.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.1205-1211
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• 2017

The Propulsion System Test Complex(PSTC) was constructed for the verification test of each stage's propulsion system of KSLV-II. Main Control System(MCS) is the system to operate the onboard equipment and the ground equipment of the PSTC simultaneously. This paper describes the critical design, the development status, and test results of Main Control System. The MCS will be used for the interface connection between ground control systems and onboard equipment. Test sequence and operation process of the Work Manager will be conducted by MCS.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.1200-1203
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• 2017

Propulsion system test complex (PSTC) is designed to verify propulsion system of KSLV-II. It is composed of hydraulic and pneumatic system, test stand system, control/measurement system, and flame deflector and safety system. In this study, kerosene filling system of hydraulic and pneumatic system is introduced. It performs store and chilling of kerosene, chilling and purging of filling line, and filling and retrieval of the kerosene. The kerosene supply requirements of 1, 2 and 3 stages of KSLV-II are considered in design process.