Author:
Kosyakov V. A.,Fursenko R. V.,Shiplyuk A. N.
Subject
Nuclear and High Energy Physics,Radiation
Reference47 articles.
1. K.K. Kuo and M.J. Chiaverini, Fundamentals of hybrid rocket combustion and propulsion, Progress in Astronautics and Aeronautics, 2007, Vol. 218. P. 1–36.
2. J. Durand, J. Lestrade, and J. Anthoine, Restitution methodology for space and time-dependent solid-fuel port diameter evolution in hybrid rocket engines, Aerospace Sci. and Technol., 2021, Vol. 110, No. 106497.
3. Y. Pal, S. Mahottamananda, S. Palateerdham, S. Subha, and A. Ingenito, Review on the regression rate-improvement techniques and mechanical performance of hybrid rocket fuels, FirePhysChem., 2021, Vol. 1, No. 4, P. 272–282.
4. C. Li, C. Kai, and H. Tian, Numerical analysis of combustion characteristics of hybrid rocket motor with multisection swirl injection, Acta Astronaut., 2016, Vol. 123, P. 26–36.
5. M. Bouziane, A. Bertoldi, P. Hendrick, and M. Lefebvre, Experimental investigation of the axial oxidizer injectors geometry on a 1-kN paraffin-fueled hybrid rocket motor, FirePhysChem., 2021, Vol. 1, No. 4, P. 231–243.