Science Links Japan | Uchu Kagaku Gijutsu Rengo Koenkai Koenshu (CD-ROM)

List of Jounal Titles

A to Z index of Journal Title. Choose a letter.

A/ B/ C/ D/ E/ F/ G/ H/ I/ J/ K/ L/ M/ N/ O/ P/ Q/ R/ S/ T/ U/ V/ W/ X/ Y/ Z/ 0/ 1/ 2/ 3/ 4/ 5/ 6/ 7/ 8/ 9

Uchu Kagaku Gijutsu Rengo Koenkai Koenshu (CD-ROM)

49th

Exploitation of Outer Space in the Interests of International Society
Current Status and Outlook of Small Satellite Research and Development in JAXA/ISTA
A trial for efficient engineering of a small satellite system
Development of Autonomous Ground Operation System for Pico-satellites
On-orbit Demonstration of Pico-satellite Deployer using M-V-6 Rocket Subpayload
Magnetic moment measurement experiments of instruments on INDEX satellite
Magnetic moment measurement and demagnetization of INDEX spacecraft
Development of Tokyo Tech pico-satellite Cute-1.7 + APD
A system consideration of a small satellite for on-orbit solar sail
Development of gas-liquid equilibrium thruster for small satellite
System Development of Spin Axis Controller for Small Spacecrafts
The motion analysis of unbalanced Yo Yo using multiparticle model
"Experiment of array-antenna construction by multi-satellite system" using S-310 sounding rocket No.36.
Study and development of the CEES rocket
Concept Design of Water/Liquid Nitrogen Rocket System
Performance evaluation of Water/Liquid Nitrogen rocket engine.
Student Hybrid Rocket Launch Experiment
Experimental Study on Wax/HTPB Hybrid Rocket Enjine
Fundamental Investigations of Micro Pulse Detonation Engine
Effects of designing of Micro-Arcjet Nozzles
Basic Study for Operating Characteristics of LASER-Electric Hybrid Propulsion
Induction Phenomena in a Laser-Sustained Scramjet
Internal Flow CFD Analysis in Combustion-Augmented Laser-Ramjets
Conceptual Study of Horizontal Launch Two-Stage Reusable Rocket Vehicles
Multidisciplinary Design Optimization of Hypersonic Experimental Vehicle
Optimal Design of Two Stage To Orbit Spaceplane Using Hybrid Genetic Algorithm
Optimization of a Flight Trajectory including separation condition for TSTO Using the Genetic Algorithm
JAXA Vison and Life Support System Technology
Technical Demonstration of Air Revitalization and Water Electrolysis System
Research & Development status for ECLSS(Environment Controlled Life Support System)
Research and Development Status of Advanced ECLSS Technology
Present status of R&D of advanced life support systems in IES
Computational Simulation of Material Circulation in CEEF
Influence of Plant and Habitation modules increase in CELSS stage construction-Using Multiagent Complex Controls-
IALSWG Charter and Plans of International Collaboration with NASA and related organizations
Commercialization of a continuous processing system for organic waste materials
Space Agriculture for Manned Mars Exploration
Construction of Solar Power Satellites Using Small Satellites
Energy Supply for moon surface missions from laser based SSPS
Study of Shaping and Control of Microwave Beam by using Multiple Transmitting Panels
Basic Experiments on DC-RF Conversion Efficiency and Frequency Spectrum of Magnetron in Continuous Run
Study on High-efficiency Microwave Power Transmission of Slotted Waveguide Power Divider
Economic Analysis of Space Solar Power Systems with JAXA's SSPS Cost Model
Future of Space Solar Power Satellite (SPS)
Overview of the USEF SSPS Activities
Summary of Studies on Space Solar Power Systems (SSPS) of JAXA
The Feasibility of Applying SSPS for Producing Commercial Power
Attitude motion of space solar power system induced by thermal deformation
Issues Related to High Voltage Bus Technology for Space Solar Power System
Risk of Space Debris Impacts on Solar Power Satellite
Arc Starting Experiments by the Space GHTA Welding using Touch Start Technique at the Space Station Orbital Pressure
Prevention Technology of Metal Vapor Deposition to Optical Device in Space Diode Laser Welding
Fillet Weld Experiments by the Space GHTA Welding Process in a Vacuum
Study of Erosion of SiC Anti-oxidation Film Coated to Carbon Material
Heating tests of C/C Composites for Extendible Nozzle with LOX/GH2 Combustion Gases (Part 2)
Atomic oxygen-induced erosion of polyimide under simultaneous e-beam exposures
Erosion of spacecraft thermal blanket materials exposed to hyperthermal atomic oxygen beam and ultraviolet ray -Comparison of fluorinated polymer and polyimide-
Influence of 5 eV atomic oxygen on the mechanical properties of high-modulus aramid fibers in low Earth orbit
Usage to Space Units of SPS Light Weight Package
Electrical Circuit Modeling for Hollow Cathode of Hall Thrusters
Sixfold Double Sheath Model of a Hall Thruster
Influences of Acceleration ChannelWall Material on Performance Characteristics and Plasma Features of Hall Thrusters
Measurement of Plasma Beam Energy Ejected from Microwave Discharge Hall Thruster
Performance Evaluation Tests of LOX/LNG Turbopumps
Observations of Cavity Fluctuations and Shaft Vibrations in Several Rocket Turbopump Inducers
Research of a Swirling Oxidizer Type Hybrid Rocket Engine for a High Altitude Rocket
Evaluation of Engine Cycles for Small Engineering Test Rocket Engine
Optimum Structural Design of Rocket Nozzle
Characteristics of Dynamic Loads on Extendible Nozzle during Altitude Change
Effects of Flow Conditions on Characteristics of Injector Elements of Liquid Rocket Engines
CFD Analysis of Rocket Plume Interactions
Long term observations for health analysis of wheels on DRTS
Results of a development test for an advanced reaction wheel with high performance
Study on the Method of Evaluating Microvibration Influence on Spacecraft Gyroscopes
A Study of On-Orbit System Identification of the Engineering Test Satellite-VIII-Estimation of a Constrained Mode Model
A case study on advanced attitude control experiments of ETS-VIII
Study of Advanced Earth Observation Satellite System Using On-orbit Servicing Shuichi Matsumoto (JAXA)
Comment on Stability of Attitude Controller With Time Delay
Real Sky Tests of Star-Tracker-Based Attitude Determination System for Earth Pointing Spacecraft
Correction of Terra spacecraft attitude fluctuation using ASTER image
Study of High Performance Fiber Optic Gyro Inertial Reference Unit
Development of a Rendezvous Laser Radar for Future Missions
System Operation Requirement for High Accuracy Positioning Experiment System
Analysis of SIS-URE of High Accuracy Positioning Experiment System Using Quasi Zenith Satellite System
Monitor Station Distribution for High Accuracy Positioning Experiment System (HiAPEX)
Time Transfer Trial for High Accuracy Positioning Experiment using Quasi-Zenith Satellite System
Time Management System for Satellite Positioning System using Quasi-zenith Satellites -Entire Structure-
Time Comparison Equipment for ETS-VIII
Preliminary Design for QZS Time Transfer Subsystem
Preliminary design of Time Comparison Unit(TCU) for quasi-zenith-satellite
Preliminary design of Time Comparison Unit(TCU) software for quasi-zenith-satellite
Time Management System for Satellite Positioning System using Quasi-zenith Satellites -Interface Design for the Ground System-
Time Management System for the Experimental Positioning System of Quasi-zenith Satellite -Connection between GPS Time and QZSS Time-
Development of internal delay calibration system in TWSTFT
Development of a Spaceborne Hydrogen Maser for QZSS
End-to-end Simulation of Remote Synchronization System for Onboard Crystal Oscillators
Feedback Control Experiments of Remote Synchronization System for Onboard Crystal Oscillators
Study on Control of Remote Synchronization System for Onboard Crystal Oscillators during Communication Interruption
The spread of the space education by cooperation with Japanese cultures
Student Initiative Projects of UNISEC Student Organization (UNISON)
Space event management from new programme
Space education for civil by students
Circuit Analysis of Solar Array Arcing on Spacecraft with SPICE
Laboratory Test of Sustained Arc between Power Cable and Back Surface of Solar Array Panel
Relationship Between Arcing Phenomena and Solar Array Coverglass Type in GEO Environment
Simulation of Internal Charging of dielectric materials for spacecraft
Development Status of the Micro Satellite "SOHLA-1"
Electrical Power System Design and Analysis for SOHLA-1
Structure Subsystem of SOHLA-1 -Design and Vibration Tests
Thermal Control System of SOHLA-1 -Design, Experiments and Analysis-
Attitude control system of SOHLA-1
Design and Development of Spin-up Wheel for SOHLA-1
Development of Boom for Micro-satellite "SOHLA-1": Development of Hinge and Dynamics of Boom
Development of Boom for Micro-Satellite "SOHLA-1": Development of Pinpuller and Vibration Tests of Boom
Tokyo Institute of Technology's Arliss2005 project
Deployment and Retrieval Strategy for Pico-Satellite "STARS-1"
Attitude Control Strategy of Engineering Test Satellite for Tethered Space Robot
Development of a computer system for Nano-Satellite
Numerical Simulation and Ground Test for Development of Superpressure Balloon
Preliminary Analysis on Equilibrium States of a Rotating Circular Solar Sail Membrane
Fundamental Research on Applicability of High Heat Resistant Polyimide for Mercury Orbiter MLI.
Tether Deployment Mechanisms of Rotationally Skew Fold Membrane for Spinning Solar Sail
Control Method of Deployment Mechanism Using Image Processing for Solar Sail Membrane Deployment
Dielectric radial line antenna using artificial dielectric radial line for inflatable structure.
The Shape of Inflatable Antenna and Recieving Experiment
Development of Film Lens Antennas for Large Aperture Radio Telescopes on Artificial Satellites
On the applicability of triaxially woven fabric composite to lightweight structures
Simple Design Method for Inflatable Parabolic Reflector Made of Triaxial Woven Fabrics CFRP -Research from Vibration Mode-
Development of Extendable Rod Using Inflation Extension Method
Study on vibration characteristic under deployment of inflatable STEM antenna system
Deployment Analysis of a New Combined Membrane Structure
Deploy Experiment of Infratable Tube using Work Hardening
A method of controlling the inflation process of the space inflatable structure
Construction of Deployable Space Structure Using Inflatable Tensegrity Modules
The research on stabilization of ultrasonic wave propagation for the ultrasonic flow meter
Basic Study on Microthrusters Using Ablation by Glow Discharge
Influences of Propellant Properties on Performance Characteristics of Solid-Propellant Laser-Ablation Thruster for Space
The Effect of the Improvement of Electrode Geometry in MPD Thruster
Study on Enhancement of Total Impulse for Electrothermal Pulsed Plasma Thruster
Performance Characteristics of a Pulsed Plasma Thruster with Parallel Electrodes and a Supersonic Nozzle
Numerical simulation of a plasma behavior to time-varying external electromagnetic field
Influence of Potential Arrangement on the Operation of Ion Engine in a Vacuum Tank
Research Status of High Specific Impulse Microwave Discharge Ion Engine .MU.10HIsp
Electron Emission Characteristics of Hollow Cathode Neutralizers
Remote sensing for Upper atmosphere with Ion Thruster
Research on microwave ion engine using antennas (2)
Development of the Microwave Discharge Ion Engine .MU.20
Three-Dimensional MHD Simulation of Magneto Plasma Sail
Numerical Simulation of Magneto Plasma Sail Using 3D hybrid code
A Concept of Multiple Access Test and Observation Facility (MATOF)
JASMINE(Japan Astrometry Satellite Mission for INfrared Exploration) Project
Design of Cryogenic System for Next Space Infrared Mission "SPICA"
Results of initial operation of SUZAKU
Initial Operation Result of ASTRO-E2 (SUZAKU) Attitude and Orbit Control System
Thermal Design of The Scientific Satellite ASTRO-E2SUZAKU
Development of Extensible Optical Bench for next generation X-ray astronomy satellite
Firing tests of a Rocket Combustor for Combined Cycle Engine at Various Conditions
Design of Sub-scale Rocket-Ramjet Combined Cycle Engine Model
Ramjet-mode Operation in a Combined Cycle Engine Combustor
Geometrical Effects of the Sidewall-Compression Type Scramjet Inlets
Application of Injection Cooling Method for Reentry Vehicles
Heat-resistance Experiments of New Ceramics by High-temperature Plasma-jets
Ingredient Alteration of Metal by High Temperature Plasma Flow and Its Flow Field
System Description of "HAYABUSA" Asteroid Explorer
System Consideration of Tethered Sampling for Minorbody Exploration in Deep Space
Localization over Small Body Surface by Radio Ranging
Modeling and Dynamics of the Planetary Airship System(PLAS)
Micro Plane for Mars Explorat ion Using Energy Transmission
Heat Shield Design for Small Solar Probe Mission
The Characteristic Study of 1/1 scale High Gain Antenna for Mercury Magnetospheric Orbiter
A Study on Guidance and Control System for Precise Lunar Landing
A Study on Visual Obstacle Detection with Super-Resolution
Research of Landing Gear Subsystem for Lunar Lander
Experimental Study of the Impact Force of the Landing on Lunar Surface
Development of a Multi-Utility Spacecraft Charging Analysis Tool (MUSCAT)
ESD Ground Test of Solar Array Paddle of OICETS
Development of Regenerative Fuel Cell for Stratospheric Platform Airship
Development Status of Power Processing Unit for 200mN-class Hall Thruster
Remote of Control of Ground Station for Small Satellites with Time Delay
Autonomous Fault Diagnosis System for Satellites based on Model Based Inference
Research on Contact Dynamics Modeling for Capturing Free-flyng Target with Manipulator in Space
Optimization of time to switch the manipulator's drive Joint using time sharing motion control
Proposal of Practical Deployable Tensegrity Module
Basic study of rotation system using eddy current for liquid wheel
Study on Fundamental Characteristic of Very Long Tether System
Optimal trajectory analysis of Turn over Problem of Tether Satellite System
Accurate Stereo Measurement by using Shadow for Sampling Task
A Three-dimensional MHD Analysis for a Magneto Plasma Sail
Cost Analysis of Transportation System of Solar Power Satellite
Perturbation Analysis of Interplanetary Sun-Synchronous Orbit
Formation Changing for Formation Flying Satellite with Measurement Errors
Development of micro satellite in Kyushu University
Aero Brake Version of QTEX
Technology Demonstration on University of Tokyo's pico-satellite "XI-V"
Development of University of Tokyo's remote sensing pico-satellite "PRISM"
About Nano-satellite for Infrared Astrometry (Nano-JASMINE) Project
Hokkaido Satellite Project: CubeSat System Launched as M-V-7 Sub-Payload
Hokkaido Satellite Project: Separation System for Cubesat mounted in Sub-Payload of M-V-7
Hokkaido Satellite Project: Development of a magnetic torquer rod for Cube Sat
Hokkaido satellite project : Research of optical communication system for small satellite
The Hokkaido satellite project: Application to agricultural sector where hyper spectrum camera was used
Hokkaido Satellite Project: Development of the Hyper Spectrum Camera
Research of Image Stabilization System for Small Satellite
Development of Precise Orbit/Clock Determination Software for GPS/GNSS
The effects of GPS positioning accuracy by QZSS
Constellation Design of Regional Satellite Positioning System
The Benefits of Three Frequencies for the High Accuracy Positioning
Study on Near Real Time Tropospheric Delay Estimation
Prototype Evaluation of QZSS Submeter-Class Wide-Area Diaerential Corrections
Experimental Results of Decimeter class WDGPS
Development of Pseudo-QZS and Evaluation Using a Helicopter
A study on the optical measurement and analysis for satellite visibility under urban environments
Study of supervising system for train operation by using QZS
Application of Satellite Communications for Supporting Medical Treatment in the Aftermath of Disasters
Studies on Subjects Related to Quasi-Zenith Satellite System in SG4 of ITU-R
Development of the Engineering Test Satellite-VIII Boarded Deployable Radiator - State of Development
Development of DPR for ETS-VIII; Result of Ground Test of DPR
Development of ETS-VIII Boarded Deployable Radiator - Evaluation of Performance Variation
Estimation of Non Condensable Gas on Loop Heat Pipe of Engineering Test Satellite VIII
Heat Transfer Characteristics of Flexible Loop Heat Pipe for Deployable Radiator on ETS-VIII
Feasibility Study on the Cooling of High Heat Generation Space Systems
Development of High Performance Cold Plates for Space
A Study on Nucleate Boiling Heat Transfer Enhancement by Thermal Spray Coating (Experimental results of pool boiling under microgravity)
Thermal design and evaluation test on flat plate evaporator with communication wick for space system
Multidisciplinary Optimum Design for Lower Weight Space Heat Rejection Radiator
Development of CFRP Faceskin Heat Pipe Panels for ETS-VIII
R&D on Space Debris in JAXA/ISTA
Detection of Small LEO debris Using CCD Sensor
Estimate of rotational motion of LEO debris and so on by optical telescope
Evaluation of Asteroid Detection Software
Performance Evaluation of Debris Shield using Polymeric Materials
Study on the Position Detection of a Space Debris Impact via Microwave Correlation
Microwave Emission due to a Space Debris Impact onto the Exposed Materials of a Space Station
The Relation Between Target Destruction Due to Hypervelocity Impact and Microwave Radiation
Test of solar array arcing through plasma induced by pseudo space debris impact using YAG laser
Damage Evaluation of Impact Feature by Debris on The Solar Cell
A Study on the Deorbit of Small-Satellites using Electrodynamic Tether
Design of electrodynamic tethers for debris de-orbit
Numerical Simulations on the Stable Tether Deployment prior to the Activation of the Conductive Tether System
Orbit Determination of Tethered Satellites by Ground Observations Using an Electric Wave Interferometer
Orbit Determination Analysis of Hayabusa just before the Rendezvous with Itokawa
Low-Thrust Stationary Orbits in the Restricted Three-Body Problem
Design of Reference Lissajous Trajectories around L2 Point in the Sun-Earth System
Optimization of Trajectories from Earth to L2
Analysis of Low Energy Interplanetary Transfer Trajectory Using Libration Points
Three-Dimensional Minimum Fuel Trajectory by Low Thrust Propulsion System
Preliminary Study on the Orbit Planning of Post-Hayabusa Asteroid Explorer Mission
System design concept for next generation spacecraft
Study of Spacecraft OBS Verification Environment Using MPU Instruction Set Simulator
Can Satellite Communications Survive?
An Ultra-Lightweight Large Antenna Reflector and an Ultra-multi Beam Feed System Onboard Future Large Mobile Communication Satellites
The Development of Variable Radiation Pattern Antenna for Satellite
Study of an Ultra Low Profile Dipole Antenna with an Increased Parasitic Part
Development of Onboard Software Defined Radio Equipment
Data bus architecture for the next generation advanced satellite
Current Status of SERVIS Project
Evaluation of Orbital Results from SERVIS-1 INU
Development of Advanced Paddle Drive Mechanism (APDM), and the result of on-orbit experiment
Feasibility Study of the Environmental Tolerance of Hard Disk Drives
Start-up Behavior of Double-condenser design Loop Heat Pipe for MAXI
Study of flexible beam carrying by a robotic arm equipped satellite
Feasibility Study on Small Hypersonic Research Vehicle using Sounding Rocket
Experiment of Liquid Transfer of Channel Mesh Accumulator Core under the gravity and atmosphere
Development of Practical Color Marker and Its Performance Evaluation Under Pseudo-Orbital Environment
Numerical Analysis of Shock Interaction around Two-Body Configurations
Lithium-ion Battery Chassis which is made of light weight and high heat Conduction CFRP
Study on Transportation of Flexible Payload using Flexible Space Robotic Arm with Redundant DOF
Experimental Analysis of Hypersonic Shock Interaction Flowfield in Two-Body Configurations
Development of a Variable Emittance Radiator (2)
Ground Experiment Testbed for Cooperative Dexterous Robot System
Fundamental Research of Fully Reusable Launch Vehicle using RPV
Application of a Simplified 3-D Thermal Modeling Method for a Whole Reentry Vehicle
An Application of Slant-axis multijoint manipulator for Welfare fields
Development Plan of a Small-scale Supersonic Unmanned Airplane in Universities' Collaboration
Mechanical Test Results of the Wideband InterNetworking engineering test and Demonstration Satellite (WINDS) System Structure and Thermal Model
Rocket Launch Operation Support System by Web Service Agent
Coupled Load Analysis and Testing Method for Evaluating Design of Satellite/Rocket
The Diagnosis of Rocket Launch Equipments using Ontologies
Aerodynamic design and wind tunnel tests of a small-scale supersonic unmanned plane
Vibration control of small satellite by sticking multilayer damping material
Third Generation Spacecraft Management and Control System and Future Conception
Flight Trajectory Analysis of a Small-Scale Supersonic Unmanned Vehicle
A Simplified Vibration Model for Initial Study of a Spaceplane
Software Development of Ion Thruster Control Unit for Deep Space Probes
The flight experiment of small-size Parafoil from a balloon for future autonomous flight
Frequency-Domain Noise Separation with Variable Structural Parameters
Proposal of New Space Transport System-Conceptual study of Hybrid Re-Entry Vehicle
Development of No-Shock Hold Release Mechanism
Development of the System to Configure Source Information for Operation Procedure
Drop Test for Recovery System using Membrane Aeroshell
Development of a High Accuracy Deployable Modular Antenna Structure for VSOP2 Mission
Anomaly Detection Methods for Spacecraft based on Knowledge Discovery by Telemetry Data Mining
Aerodynamics of Balloon-based Operation Vehicle
A study of electrical characteristics for a mesh antenna design method to reduce variations of cable tensions.
Spacecraft diagnosis method by fusion approach of knowledge and learning with data
Autonomous distributed diagnosis system for Space Solar Power Satelite -Calability Analysis Towards Actual System Size-