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Experimental Investigation of a H2O2 Hybrid Rocket with Different Swirl Injections and Fuels
Manuel Stella, Lucia Zeni, Luca Nichelini, Nicolas Bellomo, Daniele Pavarin, Mario Tindaro Migliorino, Marco Fabiani, Daniele Bianchi, Francesco Nasuti, Christian Paravan, Luciano Galfetti, Attilio Cretella, Rocco Carmine Pellegrini, Enrico Cavallini and Francesco Barato Applied Sciences 14(13) 5625 (2024) https://doi.org/10.3390/app14135625
Experimental Investigation of a Swirling-Oxidizer-Flow-Type Hybrid Rocket Engine Using Low-Melting-Point Thermoplastic Fuel and Oxygen
Measurement of Gas Flow Rate at Gasification of Low-Melting Materials in a Flow-Through Gas Generator
Dmitry A. Vnuchkov, Valery I. Zvegintsev, Denis G. Nalivaichenko and Sergey M. Frolov Energies 15(15) 5741 (2022) https://doi.org/10.3390/en15155741
Pseudo-Two-Dimensional Modeling and Validation of a Hybrid Rocket Combustion Chamber
Elena Quero Granado, Jouke Hijlkema, Jean-Yves Lestrade and Jérôme Anthoine Journal of Propulsion and Power 38(6) 957 (2022) https://doi.org/10.2514/1.B38682
Regression Rate Design Tailoring Through Vortex Injection in Hybrid Rocket Motors
M. Franco, F. Barato, E. Paccagnella, et al. Journal of Spacecraft and Rockets 57(2) 278 (2020) https://doi.org/10.2514/1.A34539
Combustion enhancement of hydroxyl-terminated polybutadiene by doping multiwall carbon nanotubes