Browse > Article

Development of Performance Analysis Program for Gas Generator Cycle Rocket Engine  

Cho, Won-Kook (한국항공우주연구원 엔진팀)
Park, Soon-Young (한국항공우주연구원 엔진팀)
Seo, Woo-Seok (한국항공우주연구원 엔진팀)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.12, no.5, 2008 , pp. 18-25 More about this Journal
Abstract
A performance analysis program has been developed for the gas generator cycle liquid rocket engine. This program predicts the system performance with the performances of subsystems which are evaluated by the models based on another analyses or experiments. The analysis method has been validated by comparing the engine performance against the published conceptual design. The performance models of the subsystems have been verified to give reasonable results by comparing with the MC-1 engine design and the system analysis of 10 ton thrust engine. The system performance of the 30 ton thrust rocket engine using LOx/Jet-A1 has been presented as an application example.
Keywords
Gas Generator Cycle; Specific Impulse; Liquid Rocket Engine; Systems Analysis;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
연도 인용수 순위
1 Goertz, C., 'A modular method for the analysis of liquid rocket engine cycles,' AIAA 95-2966
2 Miyajima, H., Nakahashi, K., Yanagawa, K. and Fujita, T, 'Specific impulse analysis of the LE-5 engine,' AIAA-84-1224
3 Shelton, J.D., Frederick Jr., R.A. and Wilhite, A.W., 'Launch vehicle propulsion design with multiple selection criteria,' J. Spacecraft and Rockets, Vol.43, No.4, 2006, pp.893-902   DOI   ScienceOn
4 http://www.spreadsheetworld.com
5 Huzel, D.K. and Huang, D.H., 1992, Modern engineering for design of liquid- propellant rocket engines, AIAA
6 KSLV-I report (IV), 2005
7 임병직, 김종규, 강동혁, 김홍집, 김희태, 한영민, '재생냉각 연소기용 구리합금과 연료 적합성 검증시험,' 한국추진공학회 2006년도 춘계학술대회 논문집, 2006, pp100-109
8 박순영, 남창호, 조원국, '액체로켓 엔진 Energy Balance 문제 해결을 위한 프로그램 개발,' 제27회 한국추진공학회 추계학술대회논문집, 2006, pp.135-138
9 Humble, R.W., Henry, G.N. and Larson, W.J., 1995, Space propulsion analysis and design, McGraw-Hill
10 O'Brien, C.J. and Ewen, R.L., Advanced oxygen-hydrocarbon rocket engine study, NASA-CR- 161748, 1981
11 Cai, G., Tong, X., Zheng, Y. and Fang, J., 'Generic optimization of system parameters for liquid rocket engine with gas generator cycle,' AIAA 2005-3743
12 조원국, 가스발생기 사이클 로켓엔진의 비추력 평가, KARI-RET-TM-2006-009, 한국항공우주연구원
13 양승호, 김희태, 강동혁, 안규복, 서성현, 한영민, 최환석, 2007, 실물형 재생냉각 액체로켓엔진 연소기(확대비3.5) 연소시험, 한국추진공학회 2007년도 추계학술대회논문집, pp.125-130
14 조원국, 박순영, 설우석, '막냉각이 적용된 액체로켓엔진의 비추력 최적조건,' 한국추진공학회 2007년도 춘계학술대회 논문집, 2007, pp.135-140
15 Kauffmann, J., Herbertz A. and Sippel M., 'Systems analysis of a high thrust, low-cost rocket engine,' 4th Int. Conf. on green propellants for Space Propulsion, 2001
16 McBride, B.J. and Gordon, S., 1996, 'Computer program for calculation of complex chemical equilibrium compositions and applications,' NASA reference publication 1311
17 Ballard, R.O. and Olive, T., 'Development status of the NASA MC-1 (Fastrac) engine,' AIAA-2000-3898
18 한영민, 김종규, 이광진, 임병직, 서성현, 최환석, 2007, 실물형 재생냉각 액체로켓엔진 연소기 연소시험, 한국항공우주학회 2007추계 학술발표회 논문집II, pp.1358-1361
19 Brown, N.F. and Olds, J.R., 'Evaluation of multidisciplinary optimization techniques applied to a reusable launch vehicle,' J. Spacecraft and Rockets, Vol.43, No.6, 2006, pp.1289-1300   DOI   ScienceOn
20 이진근, 김진한, '터보펌프식 액체로켓엔진의 시스템 해석,' 한국항공우주학회지 Vol.32, No.5, 2004, pp.109-115
21 서성현, 한영민, 김성구, 최환석, '연료 과농 가스발생기의 연소 가스 물성치에 관한 연구,' 한국추진공학회 2006년도 춘계학술대회 논문집, 2006, pp.118-122
22 김홍집, 조원국, 문윤완, '막냉각 모형을 이용한 액체로켓엔진 연소기의 열해석,' 한국추진공학회지 제10권 제4호, 2006, pp.85-92   과학기술학회마을
23 Sciorelli, F., Jones, M and Forde, S, 'Collaborative propulsion system analysis tool for pumpfed liquid rocket engines,' AIAA 2005-4441