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_of_the_loxlng_regenerative_cooled_rocket_engine/2016-05-16T09:59:13+09:00https://archive.ists.ne.jp/progress_in_rocket_engine_simulations_in_mhi/2016-05-16T09:59:13+09:00https://archive.ists.ne.jp/a_preliminary_design_and_analysis_for_the_le-x_turbopump/2016-05-16T09:59:13+09:00https://archive.ists.ne.jp/the_diverse_capacities_of_the_le-5b-2_engine/2016-05-16T09:59:13+09:00https://archive.ists.ne.jp/effects_of_injection_orifice_shape_on_discharge_coefficient_with_cavitating_n2o_flow/2016-05-16T09:59:13+09:00https://archive.ists.ne.jp/thermodynamic_effect_on_a_cavitating_inducer/2016-05-16T09:59:13+09:00https://archive.ists.ne.jp/the_needs_of_in-flight_experiments_for_cryogenic_propellant_behavior_interest_and_status/2016-05-16T09:59:13+09:00https://archive.ists.ne.jp/a_cfd_study_on_hydrogen_jet_combustion_in_the_afterburner_of_a_pre-cooled_turbo_jet_engine/2016-05-16T09:59:13+09:00https://archive.ists.ne.jp/operation_of_ikaros_rcs/2016-05-16T09:59:13+09:00https://archive.ists.ne.jp/quality_control_activities_of_high_pressure_gases_during_kslv-1_launch_campaign/2016-05-16T09:59:14+09:00https://archive.ists.ne.jp/overview_of_le-x_research_and_development/2016-05-16T09:59:14+09:00https://archive.ists.ne.jp/3d_les_of_the_hyshot_ii_supersonic_combustor/2016-05-16T09:59:14+09:00https://archive.ists.ne.jp/experimental_investigation_of_a_pulse_jet_engine/2016-05-16T09:59:14+09:00https://archive.ists.ne.jp/large-eddy_simulation_of_fuel_mixing_using_streamwise_vortices_in_a_supersonic_flow/2016-05-16T09:59:14+09:00https://archive.ists.ne.jp/design_and_experiments_of_a_han-based_monopropellant_thruster_using_arc-discharge_assisted_combustion/2016-05-16T09:59:14+09:00https://archive.ists.ne.jp/performance_test_of_mono-propellant_propulsion_system_based_on_hydrogen_peroxide_for_microsatellite/2016-05-16T09:59:14+09:00https://archive.ists.ne.jp/silanes_as_fuels_for_martian_ramjet_and_scramjet_engines/2016-05-16T09:59:14+09:00https://archive.ists.ne.jp/the_development_results_of_the_long_life_and_high_reliability_1n_hydrazine_thruster/2016-05-16T09:59:14+09:00https://archive.ists.ne.jp/study_on_mechanical_characteristic_of_paraffin-based_fuel/2016-05-16T09:59:14+09:00https://archive.ists.ne.jp/improve_combustion_efficiency_of_wax_fuel_hybrid_rocket/2016-05-16T09:59:14+09:00https://archive.ists.ne.jp/hybrid_rocket_performance_prediction_with_coupling_method_of_cfd_and_thermal_conduction_calculation/2016-05-16T09:59:14+09:00https://archive.ists.ne.jp/study_on_flow_inside_the__air-intake_of_ejector_jet_by_numerical_analysis/2016-05-16T09:59:14+09:00https://archive.ists.ne.jp/multi-stage_hybrid_rocket_design_for_micro-satellites_launch_using_genetic_algorithm/2016-05-16T09:59:14+09:00https://archive.ists.ne.jp/numerical_simulation_of_internal_ballistics_of_solid_rocket_with_non-uniformnon-isotropic_burning_rate_of_propellant/2016-05-16T09:59:14+09:00https://archive.ists.ne.jp/combustion_characteristics_of_adn_ammonium_dinitramide_based_solid_propellants/2016-05-16T09:59:14+09:00https://archive.ists.ne.jp/a_study_on_low_melting_point_thermoplastic_solid_propellant/2016-05-16T09:59:14+09:00https://archive.ists.ne.jp/observation_of_flame_stabilized_at_a_hydrogen-turbojet-engine_injector_installed_into_a_lab-scale_combustion_wind_tunnel/2016-05-16T09:59:14+09:00https://archive.ists.ne.jp/kinetics_and_mechanism_of_ap_combustion_initiation_a_complete_quantum_chemical_prediction_for_reactions_in_three_phases/2016-05-16T09:59:15+09:00https://archive.ists.ne.jp/le-x_prototype_main_combustion_chamber_development_progress/2016-05-16T09:59:15+09:00https://archive.ists.ne.jp/potential_applications_of_the_ceramic_thrust_chamber_technology_for_future_rocket_propulsion/2016-05-16T09:59:15+09:00https://archive.ists.ne.jp/active_dual_thrust_modulation_of_a_solid_propellant_rocket_motor/2016-05-16T09:59:15+09:00https://archive.ists.ne.jp/experimental_investigations_of_heat_transfer_processes_in_sub-_and_supersonic_part_of_the_film_cooled_high_pressure_loxh2_combustion_chamber/2016-05-16T09:59:15+09:00https://archive.ists.ne.jp/development_of_pulse_detonation_engine_initiator_using_reflector_for_large_bore_combustor/2016-05-16T09:59:15+09:00https://archive.ists.ne.jp/improvement_of_interface_tracking_method_for_the_analysis_of_free-surface_flows_with_phase_change/2016-05-16T09:59:15+09:00https://archive.ists.ne.jp/low-frequency_combustion_instability_induced_by_the_combustion_time_lag_of_liquid_oxidizer_in_hybrid_rocket_motors/2016-05-16T09:59:15+09:00https://archive.ists.ne.jp/influence_on_the_test_environment_on_the_transition_of_dual-bell_nozzles/2016-05-16T09:59:15+09:00https://archive.ists.ne.jp/system_analysis_of_rbcc_engine_applied_to_the_tsto_launch_vehicle/2016-05-16T09:59:15+09:00https://archive.ists.ne.jp/combustion_enhancement_in_scramjet-operation_of_a_rbcc_engine/2016-05-16T09:59:15+09:00https://archive.ists.ne.jp/performance_of_a_rbcc_engine_in_rocket-operation/2016-05-16T09:59:15+09:00https://archive.ists.ne.jp/progress_report_o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