Experimental Study on Cavitation Instabilities of Small Turbopump for Rocket Engine

Author:

HONG Soonsam1,CHOI Changho1

Affiliation:

1. Korea Aerospace Research Institute

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Reference12 articles.

1. 1) Kamijo, K., Yoshida, M., and Tsujimoto, Y.: Hydraulic and Mechanical Performance of LE-7 LOX Pump Inducer, J. Propul. Power, 9, 6 (1993), pp. 819–826.

2. 2) Hashimoto, T., Yoshida, M., Watanabe, M., Kamijo, K., and Tsujimoto, Y.: Experimental Study on Rotating Cavitation of Rocket Propellant Pump Inducers, J. Propul. Power, 13, 4 (1997), pp. 488–494.

3. 3) Tsujimoto, Y., Yoshida, Y., Maekawa, Y., Watanabe, S., and Hashimoto, T.: Observations of Oscillating Cavitation of an Inducer, J. Fluids Eng., 119 (1997), pp. 775–781.

4. 4) Hong, S. S., Kim, J. S., Choi, C. H., and Kim, J. H.: Effect of Tip Clearance on the Cavitation Performance of a Turbopump Inducer, J. Propul. Power, 22, 1 (2006), pp. 174–179.

5. 5) Lee, K. H., Choi, J. W., and Kang, S. H.: Cavitation Performance and Instability of a Two-Bladed Inducer, J. Propul. Power, 28, 6 (2012), pp. 1168–1175.

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