Science Links Japan | Proceedings of the Conference on Aerospace Propulsion (CD-ROM)

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Proceedings of the Conference on Aerospace Propulsion (CD-ROM)

47th

Solar pumped laser applied to magnesium energy cycle and space energy network
Cavitation Instabilities in Turbopumps for Rockets
Scramjet driven MHD power generation
Examination of the light metal combustion type Nonequilibrium Plasma Generation using magnesium
Remote Impulse Generation Using Laser Ablation
Atmospheric Pressure Dependence of Microwave Rocket's Thrust Performance
Orbital Dynamics of In-Space Laser Propulsion System
Relativistic Plasma Thrusters through High-Power Laser-Matter Interaction
Present Status of Study on Laser Fusion Rocket
Spin-off of the Laser Energy Transmission to Supply the Energy to the Ice Exploring Lunar Rover-Application to Drive a small airplane-
Proposal of Pulsed Heat Source MHD Electrical Power Generation
New Energy Source for Future Space Applications
Development of Space Nuclear Power Systems and the Lunar Base Reactor RAPID-L
Nuclear Fission Reactor/MHD Power Generation System for Deep Space Exploration
Prospect of Deep Space Transportation System
Supersonic mixing layer development behind half-width wedge
Study on Screech Generation from a Planar Jet
A numerical study on the flow field with film cooling
Xenon Loading System for ETS-VIII Ion Engine Subsystem
Development of Miniature Rectangular Ion Thruster
Effects of Magnetic Field on Thrust Performance in Microwave Discharge Ion Engine
Model of Pulsed Ion Beam-Driven Ablation Plasma
Development Status of Ion Engine Subsystem for ETS-VIII
Numerical Simulation of Magnetic Inflation by using 3D Hybrid Code
Development of an MPS simulator
Study on the Focal Condition in the Axisymmetric LSD Wave
Continuous Operational Test and Performance Enhancement of Electrothermal Pulsed Plasma Thruster by Improvement of Discharge Room Material and Structure
Development of a Dual Pendulum Thrust Stand for Two-dimensional Thrust Measurements
NOZZLE SHAPE OPTIMIZATION OF MPD THRUSTERS
The application of Disk-shaped MHD accelerator
Parallelization of a Particle Simulation Code Modeling a Hall Thruster
Development Status of 4.5kW class Hall Effect Thruster
Internal Plasma Structure Measurements of a Hall Thruster
Research and Development of Hall Thrusters in Osaka University
Demonstration of Propulsion System for Microsatellites in SOHLA-2 Project
Combustion Characteristics of Nozzleless Rocket Motors Employing a GAP/AP Composite Solid Propellant
Performance Evaluation of Multi-Nozzle Rocket with Throat Erosion
Combustion of Boron/Aluminum mixing powder
Combustion Experiment and Evaluation of a LOX Vaporization Nozzle for Swirling-Oxidizer-Flow-Type Hybrid Rocket Engines
Feasibility study on gaseous oxygen generation due to combustion of PMMA in liquid oxygen-Application to Swirling-Oxidizer-Flow-Type hybrid rocket engines-
Contributions and Problems of Numerical Simulation in Rocket Engine Development
Stability Analyses of the Radial-Mode Standing Waves in Solid-Propellant Rocket Motors Based on CFD
Evaluation of Heating Profile of High Heat Density Diffused Laser Heating system
Functionality Improvement and Heating Property Evaluation of Infrared Lamp Heating System for Thermal Resistive Structure Element Tests
Study of Axisymmetric Inlet with Innovative Variable Geometry-Evaluation of Effectiveness for Airbreathing Engine of Spaceplane-
Numerical Prediction of RBCC Engine Pumping Performance Under Sea Level Static
Development study of a sub-scale precooled turbo jet engine for flight experiments
Heat Exchanger Defrosting by Jet Impingement in Precooled Turbojet Engines
Relationship between flow and configuration of Rectangular-to-Circular Transition S-shape Duct Flow
Performance Estimation of a High Loaded Turbine for Hypersonic Turbojet Engine
Performance Evaluation of the Core Engine for a Small Pre-Cooled Turbojet Engine
Effects of Thermal Condition on the Intrinsic Flame Surface Instability between Parallel Plates
Local Gas Temperature Measurement in Combustion Chamber of Rapid Compression Machine using Two-Wire Thermocouple
Experimental Investigation of Pintle Injector Using LOX/GH2
Outline of ECO Project (Research and Technology Development in Japanese Environmentally Compatible Engine for Small Aircraft Project)
Current Status of JAXA Clean Engine Project
Research on Fan and Compressor of Environmentally Compatible Engine for Small Aircraft Project
Study on Advanced Turbine Cooling Technologies for Development of Next Generation Small Class Airplane Engines
Noise Measurement of a Turbojet Engine
Technology for Environmental Compatible Engine for Small Aircraft (ECO Engine) Project
Development of RQL Combustor for ECO engine
Development of Partial Lean staged Combustor for small Environmentally Compatible Engine
Research and Development of Low-NOx Technologies in JAXA TechCLEAN
Predict Method of Fan Flutter with 3D Unsteady N-S Analysis
Experimental and Analytical Evaluation on the Potential of an Electric Air-breathing Engine
Investigation of Wave Rotor Miniaturization
Design Study of Turbine for Pulse Detonation Combustor
Numerical simulation of aerodynamic effects of turbine blades in pulse detonation combustors
Thrust Demonstration of a Pulse Detonation Rocket System for Flight Test
Thrust Enhancement of a Partially-Filled Pulse Detonation Engine in a Vacuum Chamber
Initiation and Propagation of Detonation in a Supersonic Flow of a Combustible Mixture