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> Uchu Yuso Shinpojiumu. Heisei 14 Nendo
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Uchu Yuso Shinpojiumu. Heisei 14 Nendo
An experiment on the low-pressure combustion characteristic of the practical composite propellant.
The outline of in-position measuring system for measuring the amount of erosion of nozzle liner during the time of solid rocket motor's combustion.
The grasping of alumina impingement characteristic of the bell-type nozzle of solid rocket.
On the multi-purpose small-type N2O/Ethanol propulsion system.
On the result of a development of 500N-class two-component-type apogee engine.
The on-ground combustion test of a scramjet engine.
A research on the operation of dual-mode scramjet engine.
The performance evaluation of a variable-shape type ramjet engine.
A research of the combined cycle engine.
The influence on the injection angle in the cases of two-dimensional and three-dimensional supersonic mixing.
The three-dimensional mixing analysis by means of parallel injection of fuel in the combustion chamber of scramjet engine.
The influence of the turning injection and double injection on the supersonic combustion.
A basic research on the structure of underexpanded jet generated by rectangular nozzle.
Preliminary Design and Construction of a Supersonic Ludwieg Tube for Characterization of Space Plane Aerodynamics.
The effect of fuel-feeding form on the PDE's propulsion performance.
Development of a pulse detonation engine in Aoyama Gakuin Univ..
Research on improvement of an analytical model of "a hole in the ionosphere" and evaluation of a rocket launch method.
Laser ignition characteristics of GOX/GH2 and GOX/GCH4 propellants.
Research on rocket propulsion systems for university space educational programs in which the safety was emphasized.
Prospects of space transportation systems.
A Launch Vehicle Development Plan for Manned Space Flight.
Subjects of transportation systems for space solar photovoltaic generation.
Improvement plan for an LE-7A engine.
Three-dimensional numerical analysis of lateral force generated in a rocket nozzle.
Research on a big thrust expander engine.
Evaluation of a LOX/LNG engine high frequency combustion vibration suppression mechanism by simple acoustical test.
Combustion performance and cooling performance of a pressurization type LNG engine.
Research and development of a reusable rocket engine.
Trial manufacture and performance verification test of a reusable rocket engine injector.
Liquid propellant management of a reusable rocket experimental aircraft.
Research on health monitoring in liquid rocket propulsion systems.
Optimization of ascending fleight path and airframe design of a space plane using hybrid GA.
Development of Accurate Optimization Method of the TSTO Spaceplane-New Aerodynamics Model using CFD Method.
Integrated Optimization of Airframe Design and Flight Trajectory for Advanced Space Transportation Vehicle.
Formation evaluation of a perfectly reusable space transport.
Numerical analysis of flows around an airframe in separation of a two-stage space plane.
Aerodynamic interference flow field between a delta wing and a sphere head cylinder in the hypersonic region.
Development and research plan of the ATREX engine for a two-stage space plane.
System examination of the ATREX engine for flight demonstration.
Examination on angles of attack characteristics improvement of an axisymmetric intake.
Research on performance improvement of a supersonic air intake in passing through subsonic speed regions.
Research on boundary layer control on a compressive surface of a supersonic intake.
Experiment and research on frosting reduction of a very low temperature air precooler by liquid phase mixing of condensable substances.
Phase 1 flight experiment of High Speed Flight Demonstration.
Scramjet flight test plan by HyShot.
Wind tunnel experiment of aerodynamic properties of ATR engine flying test bed (EFTB).
Research and development of pulsed plasma thruster for installing on .MU.-LabSat II.
Design and operating characteristics of coaxial PPT.
Propulsive performance of liquid propellant PPT.
Improvement of thrust stand for measuring minute thrust.
Discharge characteristics of laser-assisted small PPT.
Thermal properties of Hall thruster.
Propulsive performance and ion beam measurement of Hall thruster.
Performance prediction of the Hall thruster flow field by simple one-dimensional calculation.
Microwave-Discharge Hall Thruster.
Discharge oscillatory phenomenon control in Hall thruster.
Control of discharge oscillation in Hall thruster.
Study of permanent-magnet-type Hall thruster.
Micro Satellite De-Orbiting with Solar Thermal Propulsion.
Spectral analysis of inside of minute electric power arc jet thruster.
Working characteristics of a small thruster using ablation by semiconductor laser.
Study of small microwave ion engine.
Axisymmetric surface wave excitation microplasma thruster.
Diagnosis of plasma flow field of MPD arcjet.
Basic properties of low-power applied-field MPD arcjet.
Electromagnetic force evaluation and magnetic Laval nozzle effect in MPD outlet.
Ion heating in high-speed plasma flow and application to thruster.
Study of helicon wave plasma source for next generation electric propulsion.
Laser rocket propulsion from the viewpoint of laboratory laser plasma studies.
Effect of plasma position in laser beam on performance of CW laser thruster.
Effect of propellant on operation of CW laser thruster.
Effects of sound velocity and pressure of operative gas in laser-driven in-tube accelerator.
Experiment to obtain energy dependence of propulsive performance in laser thruster using liquid droplets as propellant.
Study of performance control of orbit transfer machine by laser propulsion. Possibility of specific impulse control.
Basic experiment of microwave propulsion.
Microwave discharging oxygen plasma source for ionospheric plasma simulator.
Observation of fast neutral particles of ion engine origin.
Electromagnetic fluid analysis of MagnetoPlasma Sail.
Study of solid particle acceleration using the colloid thruster system.
Spectrometry of plasma cloud.
Study of deorbit system by electrodynamic tether on elliptical orbit.
Ground study of electron collection of bare tether.
Current status of developmental study of electrodynamic tether and electron inflow theory in U.S.A.
Flight preparation of the MUSES-C ion engine system.
Microwave discharge type ion engine .MU.20.
Microwave discharge type ion engine family: .MU.10, .MU.20 and .MU.10HIsp.
Study of microwave discharge type ion engine using slot antenna.
Application study of ion thruster to probes.
Propellant selection for ion engine supposing large-scale transportation.
Study of effect on plasma layer composition by ion thruster discharge plasma.
Air Breathing Ion Engine(ABIE:eibi).
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