
Research on the comparative analysis of thrust and specific impulse performance - different cycle types of liquid rocket engines
- 1 University of Bristol
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Abstract
As one of the most crucial parts of deep space exploration and interstellar colonisation in the global space industry, the development of rocket engines plays a vital role. The subject of this study is to investigate the effect of different cycling methods on the thrust and specific impulse of liquid rocket engines. The study will cover seven typical cycle methods and hopes to contribute to the subsequent development of more efficient and reliable liquid rocket engines, provide designers and engineers with a reference for optimising design and performance, and provide the basis for other future research in related fields that will have a profound impact on the space industry.
Keywords
thrust, impulse, liquid rocket engines, cycle methods
[1]. Zhou, C. et al. (2022) Comparison between the dynamic characteristics of electric pump fed engine and expander cycle engine. Beijing, China: Beihang University.
[2]. Soller, S., Boronine, E., Kniesner, B., & Wiedmann, D. (2014). Thrust chamber technology investigation for expander-cycle engines. In Space Propulsion Conference.
[3]. Sippel, M., Herbertz, A., Burkhardt, H., Imoto, T., Haeseler, D., & Götz, A. (2003). Studies on expander bleed cycle engines for launchers. In 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit (p. 4597).
[4]. Kwak, H. D., Kwon, S., & Choi, C. H. (2018). Performance assessment of electrically driven pump-fed LOX/kerosene cycle rocket engine: Comparison with gas generator cycle. Aerospace Science and Technology, 77, 67-82.
[5]. Davis, J., Campbell, R., Davis, J., & Campbell, R. (1997). Advantages of a full flow staged combustion cycle engine system. In 33rd Joint Propulsion Conference and Exhibit (p. 3318).
[6]. Bumb, A., & HAWK, C. (1993, June). History of staged combustion cycle development. In 29th Joint Propulsion Conference and Exhibit (p. 1939).
[7]. Kwak, H. D., Kwon, S., & Choi, C. H. (2018). Performance assessment of electrically driven pump-fed LOX/kerosene cycle rocket engine: Comparison with gas generator cycle. Aerospace Science and Technology, 77, 67-82.
[8]. Stechman, C., Woll, P., Fuller, R., & Colette, A. (2000, July). A high-performance liquid rocket engine for satellite main propulsion. In 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit (p. 3161).
[9]. Casiano, M. J., Hulka, J. R., & Yang, V. (2010). Liquid-propellant rocket engine throttling: A comprehensive review. Journal of propulsion and power, 26(5), 897-923.
[10]. Huzel, D. K., & Huang, D. H. (1967). Design of liquid propellant rocket engines (No. NASA-SP-125).
[11]. Huzel, D. K. (1992). Modern engineering for design of liquid-propellant rocket engines (Vol. 147). AiAA.
Cite this article
Mao,M. (2023). Research on the comparative analysis of thrust and specific impulse performance - different cycle types of liquid rocket engines. Applied and Computational Engineering,25,261-266.
Data availability
The datasets used and/or analyzed during the current study will be available from the authors upon reasonable request.
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Volume title: Proceedings of the 2023 International Conference on Functional Materials and Civil Engineering
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