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====== Motores Micro Híbridos e Híbridos ======

**Design Optimization and Launch of a 3" Diameter N2O/Aluminized Paraffin Rocket**, stanford University.\\
{{:acemu:bibliografia:coheteria:motores:hybrid_rocket_aiaa_paper.pdf|}}

**DAGA_MECH_FA_01 Microhybrid Rocket - Descripción y Diseño**.\\
{{:acemu:bibliografia:coheteria:motores: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.\\
{{:acemu:bibliografia:coheteria:motores: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.\\
{{:acemu:bibliografia:coheteria:motores: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\\
{{:acemu:bibliografia:coheteria:motores: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.\\
{{:acemu:bibliografia:coheteria:motores: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).\\
{{:acemu:bibliografia:coheteria:motores:the_starting_transient_in_a_gas-generator_hybrid_rocket_motor.pdf|}}


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