Advanced Hybrid Rockets for Future Space Launch
Arif Karabeyoglu
A Theoretical Prediction of Regression Rates in Swirl Injection Hybrid Rocket Engines
K. Ozawa and T. Shimada
Paraffin-based and metal-loaded HTPB fuel regression-rates study in a lab-scale hybrid rocket fed with N2O (*)
F. Scaramuzzino, C. Carmicino, G. Festa, A. Viviani and A. Russo
Development of 20 kN hybrid rocket booster
A. Bettella, F. Moretto, E. Geremia, N. Bellomo, D. Petronio and D. Pavarin
An approach to improve hybrid rocket performance
L. Galfetti, F. Nasuti, D. Pastrone and A. Russo Sorge
Design of the feed system of a Hybrid Rocket Engine
M. Demoly, J. Fissette, O. Vielpeau, A. Treilhes, N. Rizzo, J. Rčbre, J. Mulpas, V. Jacaranda-Lakiss-Marques, E. Jean-Bart and R. Mercier
Experimental Evaluation of a High Test Peroxide Catalyst Chamber for a Hybrid Rocket Engine
O. Bozic, D. Lancelle, S. May and D. Porrmann
Numerical and experimental evaluation of the performance of a cavitating valve for the control of oxidizer flow in a hybrid rocket engine.
P. Dvorak and R. Tijsterman
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