Numerical Simulation of Fuel Regression Rate Behavior of Hybrid Rocket Motors-Reference-Cited by-同舟云学术

Numerical Simulation of Fuel Regression Rate Behavior of Hybrid Rocket Motors

Published:2013 Issue:6 Volume:56 Page:351-359
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

HU Jianxin,XIA Zhixun,WANG Dequan,HUANG Liya

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/56/6/56_T-12-60/_pdf

Reference24 articles.

1. 1) Sutton, G.: Rocket Propulsion Elements, 6th ed., Wiley Press, New York, 1992, pp. 502-552.

2. 2) Kitagawa, Y., Kitagawa, K., Nakamiya, M., Kanazaki, M. and Shimada, T.: Multi-Stage Hybrid Rocket Conceptual Design for Micro-Satellites Launch Using Genetic Algorithm, Trans. Jpn. Soc. Aeronaut. Space Sci., 55 (2012), pp. 229-236.

3. 3) Frederick Jr, R. A. and Greiner, B. E.: Laboratory-Scale Hybrid Rocket Motor Uncertainty Analysis, J. Propul. Power, 12 (1996), pp. 605-611.

4. 4) Smoot, L. D. and Price, C. F.: Regression Rate of Metalized Hybrid Fuel Systems, AIAA J., 4 (1966), pp. 910-915.

5. 5) George, P., Varkey, P. M., Krishnan, S., Ravindran, M. and Yurinuv, A. A.: Fuel Regression Rate in Hydroxyl-Terminated-Polybutadiene Gaseous-Oxygen Hybrid Rocket Motors, J. Propul. Power, 17 (2001), pp. 110-116.

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