액체로켓엔진 파워팩의 시동특성에 관한 고찰

다국어 초록 (Multilingual Abstract)

A numerical study has been conducted to investigate 1-D steady/unsteady start-up characteristics for liquid rocket engine using SINDA/FLUINT. First, to verify analysis of cryogenic fluid, the object is selected RL-10 engine, liquid rocket engine of expander cycle method. Pressure drop in the cooling jacket was modelled by including some orifice devices. As a result comparisons of numerical and experimental results, there are maximum 3.14% errors by assumptions and performance curves. Analysis of cryogenic fluid is verified for liquid rocket engine. Based on these results, analysis is performed RD-8, liquid rocket engine of staged combustion cycle method. As a result comparisons of numerical and experimental results, tendency of start-up characteristics show similar behavior. It is usable to analysis of liquid rocket engine.

목차 (Table of Contents)

• Nomenclature ⅲ
• List of Figures ⅳ
• List of Tables ⅵ
• 1. 서 론 1
• 1.1 연구 배경 및 목적 1
• 1.2 국내외 연구 동향 4
• 1.3 액체로켓엔진 추진제 공급 방법 7
• 2. 지배방정식 11
• 2.1 연속 방정식 11
• 2.2 운동량 방정식 11
• 2.3 에너지 방정식 12
• 3. 팽창식 사이클 수치해석 13
• 3.1 해석 대상 13
• 3.2 모델링 16
• 3.3 결과 20
• 4. 다단연소 사이클 수치해석 27
• 4.1 해석 대상 27
• 4.2 모델링 30
• 4.3 결과 31
• 5. 결론 38
• Reference 39
• ABSTRACT 42