Regression Rate Characteristics of Paraffin-based Fuel under Swirled Oxidizer Flow
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Publisher
American Institute of Aeronautics and Astronautics
Reference5 articles.
1. 1Karabeyoglu, M. A., Cantwell, B. J., and Altman, D. "Development and Testing of Paraffin-based Hybrid Rocket Fuels," AIAA 2001-4503, 2001
2. 2Yuasa, S., Yamamoto, K., Hachiya, H., Kitagawa, K., and Oowada, Y. "Development of a Small Sounding Hybrid Rocket with a Swirling-Oxidizer-Type Engine" AIAA 2001-3573, 2001
3. Combustion Characteristics of a Swirling LOX Type Hybrid Rocket Engine
4. 4Nakagawa, I., Hikone, S., and Suzuki, T. "A Study on the Regression Rate of Paraffin-based Hybrid Rocket Fuels," AIAA 2009-4935, 2009
5. Study on the Regression Rate of Paraffin-Based Hybrid Rocket Fuels
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