1. (1) Karabeyoglu, A., Stevens, J. and Cantwell, B., Investigation of Feed System Coupled Low Frequency Combustion Instabilities in Hybrid Rockets, AIAA Paper 2007-5366 (2007).
2. (2) Karabeyoglu, M.A., Transient Combustion in Hybrid Rockets, Ph.D. Dissertation, Stanford University, Department of Aeronautics and Astronautics, Aug. (1998), pp.31-127.
3. (3) Morita, T., Kitagawa, K., Yuasa, S., Yamaguchi, S., and Shimada, T., Low-Frequency Combustion Instability Induced by the Combustion Time Lag of Liquid Oxidizer in Hybrid Rocket Motors, Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol.10 (2012), pp.37-41.
4. (4) Morita, T., Fujiwara, K., Matsuki, A., Yamaguchi, S., and Shimada, T., A Linear Stability Analysis of Hybrid Rocket Combustion (in Japanese), Proceedings of 55th Space Sciences and Technology Conference, JSASS-2011-4459 (2011) .
5. (5) Kitagawa, K. and Yuasa, S., Combustion Characteristics of a Swirling LOX Type Hybrid Rocket Engine (in Japanese), Journal of the Japan Society for Aeronautical and Space Sciences, Vol.54, No.629 (2006), pp.242-249.