Motores Micro Híbridos e Híbridos
Design Optimization and Launch of a 3“ Diameter N2O/Aluminized Paraffin Rocket, stanford University.
hybrid_rocket_aiaa_paper.pdf
DAGA_MECH_FA_01 Microhybrid Rocket - Descripción y Diseño.
mech_daga_description.pdf
Analysis and testing of similarity and scale e!ects in hybrid rocket motors, Rajeshwar Dayal Swami, Alon Gany - Instituto de Tecnología de Haifa - Israel.
analysis_and_testing_ofsimilarity_and_scale_e_ects_in_hybrid_rocket_motors.pdf
Hybrid rocket engines: The benefits and prospects, N.A. Davydenko, R.G. Gollender, A.M. Gubertov, V.V. Mironov, N.N. Volkov - Moscow FSUE “Keldysh Research Center”, Russia.
hybrid_rocket_engines_the_benefits_and_prospects.pdf
Optimum design of fiber-reinforced composite cylindrical skirts for solid rocket cases subjected to buckling and verstressing constraints, Cho-Chung Lianga,*, Hung-Wen Chenb, a Department of Mechanical Engineering, Da-Yeh University, 112. Shan-Jiau Rd., Da-Tsuen, Changhua 515, Taiwan, ROC - bInstitute of System Engineering, Chung Cheng Institute of Technology, Ta-Shi, Tao-Yuan 335, Taiwan, ROC
optimum_design_of_fiber-reinforced_composite_cylindrical_skirts_for_solid_rocket_cases_subjected_to_buckling_and_overstressing_constraints.pdf
Performance comparison between two different injector configurations in a hybrid rocket, C. Carmicino, A. Russo Sorge - University of Naples “Federico II”, Department of Space Science and Engineering “L.G. Napolitano”, P. le Tecchio 80, 80125 Napoli, Italy.
performance_comparison_between_two_different_injector_configurations_in_a_hybrid_rocket.pdf
The Starting Transient in a Gas-Generator Hybrid Rocket Motor Alexander Osherov and Benveniste Natan, Faculty of Aerospace Engineering, Technion ± Israel Institute of Technology, Haifa 32000 (Israel).
the_starting_transient_in_a_gas-generator_hybrid_rocket_motor.pdf