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)

47th

Manned space development and ISS.
The outline of the Japan Aerospace Exploration Agency (JAXA)
Current Status and Prospects of Study on Space Solar Power Systems (SSPS)
Study of configurations of the solar power satellite
SSPS System Design-Hints of Imagination
FEASIBILITY STUDY OF A SOLAR POWER SATELLITE SYSTEM CONFIGURED BY FORMATION FLYING
Investigation of SSPS Demonstration System and Future Plan
Demonstration System for Space Solar Power Satellite
Dynamic Behavior of the Space Solar Power System with Gravity-Gradient Stabilization
Orbital Feasibility Study for Space Solar Power System Demonstrator
Thermal Control System for Space Solar Power System
Study of Cold Plate for cooling transmitter using in Space Solar Power System
Cold Plate Design for Space Solar Power System
Thermal Design of Space Solar Power System Demonstration Satellite
Thermal and structure condition requested by microwave power transmission technology in SPS
Development of Panel Deployment and Latch Mechanisms
Deployable SPS Panels with SMA Actuators
Ground Experiments of SSPS Mobile Assembly Robot System in NASDA
Light-weight structural material for space solar power system
Possibility of Citizen Participation Type Space Development Support Activity
Edutainment Event Using Micro-OLIVe Mission Equipment on .MU. LabSat
Current Status and Prospects of University Space Engineering Consortium (UNISEC)-From Students' Viewpoint-
The system building and the marketing for the area education program and effective activity
Picture-Story Shows featuring Satellites
The Integrated Study Time with the Space Quiz as the In-situ Study
Science Expression Activity
NASDA Education Program on the STS-107 Space Shuttle Mission
Educational Benefits derived from International Space Station
JUSTSAP S*T*A*R*S
What is the success of the student space experiment?
Collaboration System in Educational Field
Space Moot Court Competition.
Space Education for the New Age
Significance of Exploration of Planetary Bodies and Selene-B
Geological Exploration of Lunar Surface Using a Rover
Outline of SELENE-B System Design
Technical Study on Lunar Rover for SELENE-B Mission
Navigation and Guidance Simulation for SELENE-B Lunar Landing
A Study on SELENE-B Guidance and Control System for Pin-point Lunar Landing
A Study on Obstacle Detection by Image Information
Probabilistic Obstacle Avoidance Strategy for Safe Moon Landing
Fundamental development of landing radar for Lunar and planetary mission
Research of Landing Gear Subsystem for Lunar Lander
Experimental Study on the Impact Force of Landing on the Moon
Imaging spectroscopic observations of cut sections of lunar rock-The dawn of lunar geological survey-
Experimental Verification on Optical Flow Estimation by Spatial Filter Processing using .MU.-LabSat
Examination of Tele-Driving System
Discussion of shape estimation for underground part of target sample
Discussion of Shadow-edge detection method for Shadow Range Finder
Visualization experiments of the catalyst bed of monopropellant thrusters
A study of Laser Ignition System Using Green Propellants on Cyclic Pulse Mode Tests and Synchronous Ignition Tests of Multiple Combustors.
Dynamic Behavior of Liquid Propellant in Reusable Rocket Vehicle
Observation of Combustion Flame During Chugging Instability
A Study on Flight Performance of Dual-Bell Nozzles
Heating tests of C/C Composites for Extendible Nozzle with LOX/GH2 Combustion Gases
Research on the Cause of a Nozzle Side-load Observed on the LE-7A at NAL KPL
Manufacture of a thrust stand for measurement of side-load during start-stop transients
The nozzle transverse thrust measurement test using a high altitude test facility .
Test Results on a Nozzle Side-load Problem using High Altitude Test Stand
Reusable Rocket Demonstration Vehicle System Design
Aerodynamic Design of Reusable Rocket Vehicle
The Study on ablation of thermal insulator by impingiment of high temperatuer supersonic jet
Reduction of Radiative Heating by a Carbonaceous Ablation Layer
Surface Ingredient Change of Metallic Blunt Body in Supersonic High Enthalpy Flow and The Flow Characteristics
Number Density of Atomic Oxygen in Hollow Cathode type Arc-heater
Development of a Projectile Accelerator using Supercritical Fluid
Perforation Tests and Numerical Simulations of Materials Against Space Debris Impact
Hypervelocity Impact Test on Stainless Mesh Material
Development of Structure with Self-mending Function against Space Debris Impact
Break-up Experiments due to Collision of Aluminum Honeycomb Sandwich with CFRP Skin in GEO
Evaluation and Analysis of First Retrieved SM/MPAC&SEED
Study on an Impact Detection of Space Debris via Microwave
Duty control method depending on voltage for heaters in a spacecraft
Development of Small-sized Mechanical Pump for Space
Primary Study of Lightweight Radiators for Future Space Crafts
Temperature Control due to the Operation of Vapor Valve Opening in Thermal Management System Utilizing the Latent Heat
Design analysis and Development of Loop Heat Pipe
Visualization study for Oscillating Heat Pipe by using neutron radiography
Thermal Performance Test of Oscillating Heat Pipe
Study on Cryogenic System for Next IR Astronomical Mission SPICA
Characterization of Miniature Pulse Tube Coolers for Space Applications
Development of Switching Shunt Regulator
The Development of HAYABUSA Electric Power Subsystem
Power Management of Heater Control System for HAYABUSA
Stability and control for a large-scale space power network
Prospective analysis and Approach for Human Error iin JEM development phase (Parts 2)
A Policy for the Development of Satellites introduced by a Set of Simple Models
Innovation in satellite development.
Design and application of Emergent Synthesis Environment for developing dependable system
Feasibility Study of Spacecraft Simulation Using Distributed Middleware HLA/RTI
Study on Distributed Object-Oriented Framework for Spacecraft Simulation
Research and development of Wide-band Inter-Networking engineering test and Demonstration Satellite (WINDS)
Model Driven Development of the WINDS RE-configurable Spacecraft Simulator (RESS)
Path Planning and Feedback Control for Satellite with Two Wheels
Study on formation flying of tethered satellites
Study on the optical performance of the ETS-VII rendezvous laser radar
Three-Dimensional Microgravity Environment Experiments Using a Docking Mechanism and a Nano-Satellite with Thruster
A surface erosion of polyimide in the low Earth orbit(3)-The quantification in synergistic effect on atomic oxygen and ultraviolet-
Experimental Evaluation of Cryogenic Performance for TEEK Polyimide Form Insulation
Feasibility Study of Filament Wound Composite Propellant Tank without Inner Liner
Development of Electro Rheological Fluid Damper
The Study of the Synthesis analysis of structure and control designs for the Space Open System Plan
On-Orbit System Identification Experiments on Engineering Test Satellite-VIII -Pre-Launch Verification of Feasibility and Safety of Experiments using Flight Model Software-
Experimental Properties of PVDF for Shape Control of Space Membrane Structures
The effects of launch vibration on tribological characteristics of MoS2 lubricated ball bearings
Evaluation of Tribological Properties of Space Bearing and Oil
Tribological Characteristics of Greases for Space Mechanism
Solar Paddle Driver for Small Satellites Using Shape Memory Alloy
Embedded Computer System with Soft Core CPU for Space Application
Research and Development of a High Reliable Reaction Wheel
High Density Packaging Technology for Space Units
The Test Result of High Accuracy Clock (HAC) for ETS-VIII
An experimental study of on-orbit cryogenic liquid transfer technique using swirl flow
Numerical Analysis and Ground-based Experiment of Thermal Phenomena and Fluid Behaviors in On-orbit Transfer Technique
Building Method for Expandable Material Circulation Control System of CELSS
Development of Organic Waste Material Reutilization System applied Manned Space Technologies
Miniature C Band Radar Transponder for Sounding Rockets
Satellite LASER Ranging system in NASDA
Methods for the Orbit Determination of a Tethered Satellite System by a Single Ground Station
The improvement results of the orbital accuracy for Low Altitude Satellites using E10.7 indices inputting Upper-atmosphere Models
Apogee Engine Operation of KODAMA(DRTS)
Orbit Determination of User Satellite Using Satellite-to-satellite Ranging Data via DRTS
Solar radiation pressure model of ETS-VIII
Parallel optical surveillance of near-geosynchronous orbits with high inclination
Improvement of the lunar gravitational field model using the SELENE doppler data
Mission Display for the Selenodesy using SELENE Sub-satellite Rstar by Usuda Deep Center (UDSC) Compatibility Tests
Orbit Determination Accuracy Improvement for Deep Space Missions
The Application of Noncoherent Doppler data types for the navigation of Interplanetary spacecraft
Nozomi Orbit Determination and .DELTA. VLBI Observation
HAYABUSA Orbit Determination under Low Thrust Operation
Abort Capability of Reusable Launch Vehicle
Modal Parameter Identification Intended to Construct an Unmanned Parafoil System
A study of Deep Space Missions Using Magneto Plasma Sail
Basic research on the hybrid rocket engine based on oil and fat type fuel
Investigation on the discharge instability and the performance of the Hall thruster
a study of optimization of the steering control law of flying to L4(L5) by an electric propulsion
A study on multiple fly-by to Trojan asteroids family by ballistic trajectories.
Verification of the Guidance and Control Algorithm for a Lunar Lander
Analysis of Dynamics for Electrodynamic Tethers System for Space Debris Removal
Development of an Attitude Control System for Spacecraft Using Three-Axis Attitude Control Experimental Device (1st Report, Evaluation of the Characteristics on the Experimental Device)
Development of an Attitude Control System for Spacecraft Using Three-Axis Attitude Control Experimental Device (2nd Report Experiment of Attitude Control)
Research of vibration control of large space structures using tensegrity structure
A study of a nonholonomic robot
A Study of Nonholonomic Posture Change
In-Orbit Transportation of SSPS Considering Debris Impacts and Cell Degradation by Radiation
Optical Spectrum Measurement of Sustained Arc Plasma on High Voltage Solar Array for GEO Environment
Compact Microwave Energy Transmitter
Laser Based Space Solar Power Station, L-SSPS
Earth Environment Observed by Midori-II
GLI on-orbit checkout status
Validation status of Midori-II GLI data
Operational status of Improved Limb Atmospheric Spectrometer-II (ILAS-II)
On-orbit checkout results of AMSR and AMSR-E
Data evaluation status and expected use of AMSR onboard Midori-II
In-orbit Checkout of Data Collection System (DCS) on board MIDORI II (ADEOS-II) Satellite
ARGOS Two Way Communication by ADEOS-II DCS
Web-based approach to the space education: an attempt in The Moon Station
Optical Observation Campaigns for Spacecraft for Deep Space
The new tool of crater counting: SELENE@home
Making new domestic launch site bring to horizontal competition of Space Technology
One Approach to Space Outreach Activities Using Satellites
Introduction to Tokai Student Rocket Project
On the Optimal Relationship between the Real Space Missions and Engineering Education
The Necessity of Interdisciplinary Space Education
Space Development Activities and Exploitation of Application Missions
Sample of Paper for the 47th Symposium on Space Science and Technology
Experimental Study on Photovoltaic Power Generation by Solar Concentration
Heat Transport Experiments on a Na Heat Pipe by Direct Solar Concentrating Heating
Concept of the Quasi-Zenith Satellite System Project
System Overview of Quasi-Zenith Satellite System
The Communications and Broadcasting System of the Quasi-Zenith Satellite System
A Study of the Optimal Orbit for QZSS
Optimal Orbit of Quasi-zenith Satellites for Communication Satellites and Satellite based Positioning
Feasibility Study for Ascent Trajectory of Quasi-Zenith Satellite using H-IIA Launch Vehicle
Feasibility Study of Spare Satellite Orbits for Quasi-zenith Satellite System
Considerations on Orbit Control Method for Quasi Zenith Satellite System
Feasibility Study of Pointing Control for Quasi-Zenith Satellite
A Study on Optical Observation of Quasi-zenith Satellites
Considerations on Onboard Repeater System for Quasi Zenith Satellite System
Considerations on Onboard Antenna System for Quasi Zenith Satellite System
Comparing Electrical Characteristics of Mesh Reflecting Surfaces for Mobile Communications and Broadcasting Satellite's Large Deployable Antenna
Terminal Antennas for Quasi-zenith Satellite Systems
PDE-Ram Hybrid Power Unit for Economical Space Plane
New Concept of Space Transportation System with Membrane Structure and Its High Speed Flight Test using Large Scientific Balloon of ISAS
Aerodynamic Interaction in Hypersonic Region for a TSTO Space Transport
Aerodynamic Subjects for Next Generation Space Transportation Systems
Feasibility Analysis of an ATREX Flight Demonstrator Vehicle
Building of Conceptual Design Process for Rocket-Based Two-Stage-to-Orbit
Expectation to Promotion of Research and Development of Future Space Transportation System by Cooperation of Industries, Government and Academia
A Concept of a Reentry Flight Experiment and Easy Access to the Space by Using the Reentry Vehicle
Studies for Reusable Space Transportation System
Structure Subsystem of MicroLabSat
Electrical Power Subsystem of MicroLabSat
Development of attitude determination and control subsystem of Micro LabSat
On-Orbit Operation of the .MU.-LabSat Attitude Control Subsystem
On-Orbit Attitude Estimation Experiment using CCD Earth Sensor
On-orbit Display of the Release Mechanism for SELENE Small Sub-satellite using .MU.-LabSat
In-orbit Demonstration Test for Thermal Performance of .MU.-LabSat's onboard Oscillating Heat Pipe
Result of MicroLabSat Ground Operation System
Preliminary Experiments on Orbital Maintenance System Using Micro-LabSat
Experiments of man-machine I/F during Micro-Olive mission
On-orbit Color Image Processing of an Ejected Object
Motion estimation and tracking experiments of the tumbling object using .MU.-LABSAT
Overview of Micro LabSat II
Development of Attitude Control System S/W for Whale Ecology Observation Satellite(WEOS)
Launch Report and Orbital Data Analysis of the Nanosatellite CUTE-I by Tokyo Institute of Technology
Development of Ground Station System for CUTE-I and CUTE-I Ground Operation
Missions and Concept Design of Titech Picosatellite CUTE-II
Thermal Design Method for Nano-satellites under Uncertain Thermal Conditions
Fiber and Fabric Technologies for Space Inflatable Structures
Shape Memory Polymer for Space Inflatable and Deployable Structure
On Generation of An Inflatable Paraboloidal Reflector
Inflatable Parabolic Reflector Using Membrane Rigidization Method
Configuration and its Control of Pressurized Membrane Structure
Dynamics Simulation of Pressurized Flexible Membrane Structures for External Forces
Vibration Characteristic Evaluation of Inflatable Tube with the Piezoelectric Film
Configuration effect of space inflatable supporting structure on structural characteristic
Research and development of a Large space structure using the industrial policy of the Ministry of Economy, Trade and Industry
Concept of Membrane/Inflatable-Tube Integrated Structures and Its Deformation By Internal Pressure in Deployment Process
Deployment Characteristics of The Inflatable Tube
Deployment performance of inflatable tubes which are folded by several different ways under micro-gravity.
Development of Atomic Oxygen Concentrator (2)
The laboratory test results of the space-borne quick-scanning FTS
Development of a Tip-Tilt Mirror system for "SOLAR-B"
The result of the system integration test of "HAYABUSA" multiband imaging camera
Technical note on fabrication of small integration sphere for testing multiband imaging camera(AMICA) of the HAYABUSA.
On the Orbit Transfer utilizing the Tether System Dynamics in the Debris-Crowded Circular Orbit
Orbital analysis of space debris on breakups
Hybrid Control with Minimum-impulse Transfers in the near vicinity of a circular orbit and Constant Acceleration Equivalent Trajectory Shaping
Global Optimization of the Guidance Law for a Large Number of Formation Flying Spacecrafts
A study on Cycler Orbit Between Earth and Mars
Extension of Launch Opportunity and Identical Spacecraft Design for Venus Exploration
MUSES-C(HAYABUSA) Trajectory Design
Preliminary Analysis of Jovian Aerobraking Flight Trajectories and Aerodynamic Heating
Thrust Production Mechanism of a Magnetoplasma Sail
Flight Test of Microwave Beaming Propulsion using 1MW class Gyrotron
Impulse generation mechanism in pulsed laser propulsion using droplet propellant
Application Study of Laser Propulsion on Spaceplanes
Air Breathing Ion Engine (ABIE: eibi)
Water Propelled Solar Thermal Propulsion for Micro Satellites
Study of Flight Proof Model for Water-Energy-Cycle Space Propulsion System
Preliminary experiment of non-combustible rocket engine
Control of Relative Position and Attitude of Spacecrafts using Magnetic Force
Study on Navigation and Control for "Tethered Retriever"
Intelligent Learning System for Spacecraft Attitude Control
A Study on Deployment Dynamics of Spinning Solar Sail
Analysis of reaction wheel disturbance with Air floating disturbance detector
The Research on GPS/INS hybrid navigation system using MEMS technology
Accuracy improvement of Satellite Positioning System by using HAPS
Consideration on Integrated Propulsion and Energy System
Soka University CubeSat Project
Nihon-University CanSat Project2003
A new aircraft undercarriage to prevent tire smoking on landing
In orbit AOCS performance of HAYABUSA spacecraft in cruising phase
System design and autonomous functions of the Asteroid Sample Return Spacecraft "HAYABUSA"
HAYABUSA IES Orbital Opreration
Engineering Database for ISAS Spacecraft Operation Needs (EDISON)
Orbit Control Management of Co-located Broadcasting Satellites
Advanced and plain satellites operations using event driven commands
On orbit initial checkout results of Advanced Earth Observing Satellite-II (ADEOS-II)
On orbit technical evaluation of ADEOS-II bus system
The On-Orbit Demonstration of the Optical-disk Data Recorder (ODR)
On orbit verification of ADEOS-II Inter Orbital Communication
On orbit operation results of ADEOS-II IOCS
On orbit evaluation result of ADEOS-II Solar Array Paddle (vol. 1)
On orbit evaluation result of ADEOS-II Solar Array Paddle (vol.2)
ADEOS-II orbit determination experiment using GPS data (1)
Flight Data Analysis of GPS Receivers boarded on ADEOS-II
In-Flight Evaluation of the Attitude and Orbit Control subsystem (AOCS) of ADEOS-II
In-Flight Satellite Attitude Evaluation by the Dynamics monitoring subsystem (DMS) of ADEOS-II
On-orbit System Identification of ADEOS-II
Evaluation of ADEOS-II disturbance on orbit
Inner Disturbance Analysis of ADEOS-II
USERS Project Scheme and its Evaluation as a Space Experiment Infrastructure
USERS Reentry Capsule and its Reentry Rerated Design and Flight Results
USERS on orbit, re-entry and recovery operation scheme
Orbital Operations for the Unmanned Space Experiment Recovery System (USERS)
USERS Re-entry Module (REM) System and Recovery Operation Result
First Report of READ Experiment onboard USERS Reentry Capsule
Outline and evaluation of thermal protection system for USERS/REM.
Orbit Tracking of USERS Recovery Vehicle with a High Performance Long Pulse Primary Radar
Overview and evaluation of USEF Space Operation Center
The employment plan and enforcement situation in plural experiments simultaneous operations.
Flight Operation of Large Superconductive Bulk Processing Gradient Heating Furnace
Experiment of Advanced Inertial Reference Unit
Interim Report on the On-board Computer with Automotive Technology (OBCA) Experiment in the USERS mission
Experimental Condition of the CPDR (Capillary Pumped Deployable Radiator)
On-orbit Verification of Advanced Star Sensor System (AS3)
On-orbit Experiment Report of Dual Frequency Space GPS Receiver
Considerations on Hand-over Method for Quasi Zenith Satellite System
Shadowing Evaluation for Quasi-zenith Satellite using Sun Shades of Ground Structures.
The overview of applications upgraded by the Quasi-Zenith Satellite System
Quasi-zenith Satellite Application for Telemedicine
High Accuracy Navigation Service using Quasi-Zenith Satellite System
High Accurate Navigation Experiment using Quasi-Zenith Satellite System
Study on the Performance of Positioning System Using Quasi Zenith Satellites
Plan of the Time Keeping System of Quasi-zenith Satellite System
The Accuracy of Orbit Determination and Time Synchronization for the Quasi-Zenith System (The Result of the Numerical Simulation)
Remote Synchronization System of On-board Crystal Oscillator from Ground Station-RESSOX-
Development of a Spacebone Hydrogen Maser for QZSS
Research and development of inter-satellite ranging equipment for quasi-zenith satellite System
Application study of QZS on railway systems
Optimal Orbit of Quasi-zenith Satellites for Communication and Positioning System
Present condition of Global D-GPS & Subjects of QZSS Positioning System.
The optimal success/error rate and its calculation in the resolution of integer ambiguities in the real-time-kinematic (RTK) carrier phase positioning of Global Positioning System (GPS)
3 D simulation for the improvement of GPS performance by Quasi Zenith Satellite System
Status of 150-mN Ion Engine Research at JAXA
Development of a Microwave Discharge Ion Engine using Multi-Monopole Antenna
Experiments on Ion Beam Deflection Phenomena in an Ion Thruster
Operation of Small Scale Ring Cusp Ion Thruster and It's Vacuum Test Facility
Xenon Gas Flow of an Orificed Hollow Cathode
Initial Operation of Microwave Discharge Ion Engines onboard "HAYABUSA" Spacecraft of Asteroid Sample Return Space Mission
Development of the microwave discharge ion engine .MU.20
Plume Diagnostic Measurements of a 1kW Arcjet Thruster
Evaluation of Pulsed Plasma Thruster Contamination for Small Satellite
R&D on Pulsed Plasma Thruster for .MU.-Lab Sat II-Performance Evaluation of Engineering Model-
Influence of operation time on Plume and Spot modes characteristics of Hollow Cathode
Current Collection via Plasma Cloud by Plasma Contactor
Thrust Performance of 1 kW class Anode Layer Thruster
Investigation of a Microwave-Discharge Hall Thruster
Flight and Operation Results of University of Tokyo's Nano-Satellite CubeSat XI
Report on Operation and Orbital Estimation of University of Tokyo's CubeSat
Image Acquisition Mission and Its Delivery Service of University of Tokyo's CubeSat
On the attitude motion of University of Tokyo's CUBESAT
Robotics system of asteroid surface explorer MINERVA
Principles of Hopping Locomotion in Microgravity
Mole typed Robot for Lunar Subsurface Exploration
Evaluation of Grinding Performance by Horn in Ultrasonic Grinding System
Angular Momentum Reduction using Mechanical Impulse considering Contact Force
RESEARCH ON RECONFIGURABLE AND REUSABLE CELL TYPE OF SATELLITE
On-orbit Assembly of a Large Aperture Reflector
A study of measures for deployment problems of large space structures by space robot
Numerical Analysis and Ground Experiment of Brachiation of Space Robot on Large Flexible Structure
Space robotic manipulation of massive payload considering vibration suppression
Manipulator Simulator for Conceptual Design Phase
A Ground Experimental Set-up for IVFFS
Study on Deployment Dynamics of Rolled-Up Inflatable Tube
Experimental Consideration on Membrane Deployment of Tether Controlled Spinning Solar Sail
Deployment dynamics of solar sail using centrifugal force
Characteristics of Deploying Membrane for Solar Sail on Geometrical Configuration and Fold Pattern
Finite Element Analysis of Wrinkled Membranes by Projection Matrix
Finite Element Analysis of Flexible Membrane Structures with Wrinkling
Highly Precise Paraboloidal Concentrator of Single Polymer Membrane and Its Application to Solar Thermal Propulsion
Large Displacement of Circular Membrane under Concentrated Load
An Ultra-light Large Deployable Antenna - Key Technologies and a Feasibility Study
An Ultra-Light Large Deployable Antenna.-Design Technology for a Reflector with an Ultra-Light Support Structure-
An Ultra-Light Large Deployable Antenna-Analysis and Design Technology taking account of buckling for an Ultra-Light Structure-
Influences of Thermoelastic Wave and Thermoelastic Coupling on the Dynamic Responses for Super Large Scale Space Structures
Torsional Vibration Model of Solid Rocket coupled with propellant
Microvibration Transmissibility Test of Solar-B
Development of Optical Observation Technology
Tsubasa(MDS-1) Experiment Results and Post-Operational Phase Status
Ionospheric Effects on GPS over Japan
Observation of Precipitation from Space-from TRMM to GPM-
SAR Interferometry Dual Satellite System: SIDUSS 2002
the MTF evaluation method of micro-vibration on SELENE satellite
Technical Problems of Developing of The Next Generation Star Tracker
Next Generation Autonomous Star Tracker
Development of a compact sun aspect sensor
Characteristics of High Gain Antenna by Half Size Model for Mercury Orbiter
The Characteristics of S-band Antenna for INDEX Satellite
Circular Polarization Antenna for Small Satellite
Fundamental Study for Contoured Beam Antenna Consisting of Cable Networks
An Experimental Evaluation of Stable Platform for High Accuracy Auto-Tracking Antenna System
Mobile Tracking System Experiments using Optical Sensor (part3)
Application to the satellite Communication equipment of Software Defined Radio
Development of the prototype On-board Software Defined Radio
An Overview of the High Speed Flight Demonstration Project Phase I
Results of Actual Flight and Evaluation for Guidance and Control System of High Speed flight Demonstration Phase II
Application of Multi-Disciplinary Simulation for the Development of Future Re-usable Space Transport Systems
Multidisciplinary Optimization of Space Plane Using Approximation Method
Optimum Design for a Two-Stage-To-Orbit (TSTO) Spaceplane Using the Genetic Algorithm
Performance Analysis of Partial-Reusable Launch Vehicles
Experimental Study on Winged SSTO Configuration Design