Combustion Tests for the Gas Generator of a 7 tonf Class Liquid Rocket Engine using Industrial Flow Control Valves

Byoungjik Lim; Hyeon-Jun Kim; Munki Kim; Jonggyu Kim; Hwan-Seok Choi

Combustion Tests for the Gas Generator of a 7 tonf Class Liquid Rocket Engine using Industrial Flow Control Valves

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산업용 유량제어밸브를 이용한 7톤급 액체로켓엔진 가스발생기 연소시험

Type: Proceeding

Author: Byoungjik Lim (한국항공우주연구원) Hyeon-Jun Kim (한국항공우주연구원) Munki Kim (한국항공우주연구원) Jonggyu Kim (한국항공우주연구원) Hwan-Seok Choi (한국항공우주연구원)

Journal: The Korean Society of Propulsion Engineers 한국추진공학회 학술대회논문집 한국추진공학회 2013년도 제41회 추계학술대회 논문집

Published: 2013.12

Pages: 187 - 190 (4page)

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Combustion Tests for the Gas Generator of a 7 tonf Class Liquid Rocket Engine using Industrial Flow Control Valves

Research history (16)

2020

Development and Acceptance Test Results of 75-tonf Class Liquid Rocket Engine Gas Generator

Byoungjik Lim , Munki Kim , Donghyuk Kang and others 3 Journal of the Korean Society of Propulsion Engineers 2020.08 Academic journal

2019

Development and Acceptance Test Results of 75-tonf Class Liquid Rocket Engine Gas Generator

Byoungjik Lim , Munki Kim , Donghyuk Kang and others 3 한국추진공학회 학술대회논문집 2019.11 Proceeding

2018

Operating Margin for the Gas Generator of a 75-tonf Class Liquid Rocket Engine

Byoungjik Lim , Byeongyong Lee , Hwan-Seok Choi 한국추진공학회 학술대회논문집 2018.12 Proceeding

2016

Current Development Status of 75-tonf Liquid Rocket Engine Gas Generator for KSLV-II

Byoungjik Lim , Munki Kim , Jong-Gyu Kim and others 1 한국추진공학회 학술대회논문집 2016.12 Proceeding

2015

Hot Firing Tests of a Gas Generator for Liquid Rocket Engine using a Turbine Manifold Simulator

Byoungjik Lim , Munki Kim , Jonggyu Kim and others 1 Journal of the Korean Society of Propulsion Engineers 2015.10 Academic journal

Hot Firing Tests of a Gas Generator for Liquid Rocket Engine using a Turbine Manifold Simulator

Byoungjik Lim , Munki Kim , Jonggyu Kim and others 1 한국추진공학회 학술대회논문집 2015.05 Proceeding

2014

Combustion Tests of the Gas Generator Development Models of a 75 tonf-class Liquid Rocket Engine

Byoungjik Lim , Munki Kim , Hyeon-Jun Kim and others 3 한국추진공학회 학술대회논문집 2014.05 Proceeding

2013

Combustion Tests for the Gas Generator of a 7 tonf Class Liquid Rocket Engine using Industrial Flow Control Valves

Byoungjik Lim , Hyeon-Jun Kim , Munki Kim and others 2 한국추진공학회 학술대회논문집 2013.12 Proceeding

2012

Conceptual Design and Manufacturing Scheme of a Gas Generator for 7 tonf Class Rocket Engine

Byoungjik Lim , Moonki Kim , Donghyuk Kang and others 1 한국추진공학회 학술대회논문집 2012.05 Proceeding

2011

Low Pressure Firing Tests of 75-tonf-Class Channel Cooling Thrust Chamber

Byoungjik Lim , Yeoung-Min Han , Jong-Gyu Kim and others 1 Journal of the Korean Society of Propulsion Engineers 2011.02 Academic journal

2010

Preliminary Design of Test Facility for 75-tonf-Class Liquid Rocket Engine Combustor

Byoungjik Lim , Seonghyeon Seo , Munki Kim and others 3 Journal of the Korean Society of Propulsion Engineers 2010.10 Academic journal

Low Pressure Firing Tests of 75-tonf-Class Channel Cooling Thrust Chamber

Byoungjik Lim , Yeoung-Min Han , Jong-Gyu Kim and others 5 한국추진공학회 학술대회논문집 2010.05 Proceeding

2009

Preliminary Design of Test Facility for 75 tonf Class Liquid Rocket Engine Combustor

Byoungjik Lim , Jonggyu Kim , Kwang-Jin Lee and others 6 한국추진공학회 학술대회논문집 2009.11 Proceeding

2008

Combustion Stability Evaluation of 30 ton-f Class Liquid Rocket Engine Combustor

Byoungjik Lim , Kwang-Jin Lee , Munki Kim and others 5 한국추진공학회 학술대회논문집 2008.05 Proceeding

Stability Rating Tests of 30 tonf class Regeneratively Cooled Combustor

임병직 , 이광진 , 김종규 and others 4 한국항공우주학회 학술발표회 초록집 2008.04 Proceeding

2006

Stability Rating Tests of Combustion Chamber of Liquid Rocket Engine with Baffled Injectors

임병직 , 이광진 , 김성구 and others 2 한국항공우주학회 학술발표회 초록집 2006.11 Proceeding

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Industrial flow control valves were installed to change the propellant flow rate in the combustion test facility for the gas generator of a 7 tonf class liquid rocket engine. And then their operating characteristics were investigated through cold flow tests. Two combustion tests were conducted in such a way that 3 operating conditions were covered in one ignition firing, and cyclogram was set to ensure 10 seconds steady state period for each condition. From two tests, it shows the possibility of combustion test for multiple operating conditions although there are a few things to be improved.

#Gas Generator(가스발생기) #Liquid Rocket Engine(액체로켓엔진) #Flow Control Valve(유량제어밸브) #Kerosene(케로신) #Liquid Oxygen(액체산소)

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