List of Jounal Titles
A to Z index of Journal Title. Choose a letter.
Uchu Kagaku Gijutsu Rengo Koenkai Koenshu (CD-ROM)
50th
- The Production of DVD for water-rocket
- The Mars Rover contest which connects educational fields and space development fields
- The possibility of water rocket in educational view
- Student Rocket Project at Tokai University
- Space education planned and practiced by student union
- The Alma Mater Visiting Project-Outreach Activity by UNISEC Participation Students-
- "Discover the ISS": School club activities for students featuring the International Space Station.
- Life Support Mechanism and Ecosystem
- Manned Space Mission for Space Frontier
- Human Evolution and Human Space Activities
- Study of Air revitalization system for closed ecological system
- Plants as essential elements for long-term manned space mission
- Outline of achievements in habitation experiments conducted using the Closed Ecology Experiment Facilities in 2005 and a future plan about them
- Manned Space Exploration for Post-ISS Era and Space Agriculture
- H-II Transfer Vehicle (HTV) Development Status
- Development Status of H-IIB Launch Vehicle
- Development Status of the HTV Operations System
- Development of HTV Exposed Pallet
- HTV Proximity Communication System (PROX) Preparation Status
- Results of HTV Thermal and Structure Development Tests
- Development of HTV Avionics System
- Development of HTV Propulsion System-its peculiarity and future view-
- HTV Rendezvous Flight Operation Plan
- HTV safety assessment and safety ensuring process
- Lunar landing missions and technology development status
- A Study of Obstacle Detection and Avoidance for Lunar Landing
- Development of Landing Radar for Planetary Explorer: Current Situation and Result of Field Experiment using BBM
- Lunar Science Exploration: A Top Priority Space Science Program
- Astronomical observation on the Moon
- Lunar Resource Utilization, Efforts and Technologies
- Human Lunar Activity as Part of Human Space Activity
- Technical issues and robotics on lunar survey mission
- Study of scientific instruments for the Future Lunar Exploration and Survey Mission
- Study on Lunar Exploration Rover (Actuator and Thermal Control)
- Environment and energy problem on the moon
- Space suit for Manned Lunar Activity
- Examination status of the ECLSS system for the lunar manned base in JAXA
- Robots to operate on the Human Moon Base
- Advanced Land Observing Satellite (ALOS) and Early Operation results
- On-board Gigantic Mission Data Handring for the ALOS:Initial Operation
- Design and Validation of the ALOS (DAICHI) thermal control
- Precision Attitude Determination and Control for the Advanced Land Observing Satellite (ALOS): Flight Results
- GPS Receiver and Precision Position Determination for the Advanced Land Observing Satellite (ALOS): Flight Results
- ALOS Ground Data System Commissioning Result
- Archive and distribution of Daichi (ALOS) data
- Panchromatic Remote-sensing Instrument for Stereo Mapping (PRISM): Initial Operation Results
- The development and results of the initial function check of the Advanced Visible and Near Infrared Radiometer type 2
- Preliminary Results of Calibration and Validation for ALOS Optical Sensors (PRISM and AVNIR-2)
- Development and Initial Check Out Summary of Phased Array Type L-Band Synthetic Aperture Radar PALSAR
- PALSAR calibration results
- Laboratory Demonstration of the upper atmosphere observation using artificial Ion beam
- A Software Package Development for Estimating Atmospheric Path Delay based on Numerical Weather Prediction Model
- Roles of Space Utilization in Disaster Management
- The development of a small satellite for measuring the space environment
- Multidisciplinary Design Optimization of Hypersonic Experimental Vehicle for Ballistic Flight
- Estimation of aerodynamic characteristics of Fully Reusable Launch Vehicles by Flight tests
- Influence of Engine Switching Conditions on SSTO by Changing of Body Characteristics
- A study of gas jet interaction improvement in space orbiter
- A Study of Reduction of Aerodynamic Heating on Infinite Catalytic Wall with Secondary Flow
- Experimental Research on Wax-based Solid Fuel for Hybrid Rockets
- On the Development of Reusable Launch Vehicles
- The Development of pico-satellite SPROUT
- Development of flight model of micro space satellite HIT-SAT
- CubeSat "SEEDS" Launch Report
- On-orbit Demonstration Plan using Small Demonstration Satellite in JAXA
- Thermal and Structural Design of HIT-SAT
- Thermal Control System of Small Satellite "QSAT"
- Thermal Design of The infrared astronomy satellite ASTRO-F "AKARI"
- Development of a Reversibly Deployable Radiator for Spacecrafts (1st Report: Thermal Investigation for Venus Orbiter, PLANET-C)
- Development of a Reversibly Deployable Radiator for Spacecrafts (2nd Report: Structure and Mechanism Investigation for Venus Orbiter, PLANET-C)
- Estimation of an Effective Emittance of Multilayer Insulation-Measurement with a Boil-off Calorimeter-
- Study of Motion Control of Space Elevator
- Motion estimation of a malfunctioned satellite using 3D shape model
- Nonlinear Dynamics of Tape Tether with Bending and Twist
- NUMERICAL ANALYSIS AND EXPERIMENT OF A RIGID BODY BY A TETHER IN TWO DIMENSIONS
- Measurement of Ejector Generated by Hyper-Velocity Impact Experiment
- Assessment for arc plasma characteristic on solar array in GEO environment
- Calculation of Flows in an Inductively Coupled CO2 Plasma Wind Tunnel
- An Atomic Number Density Distribution in a Xenon Hall Thruster Plume
- Development of a Dual Pendulum Thrust Stand
- Study of Shape Optimization about MPD Thruster Nozzle
- Time-resolved measurement of laser ablative impulse generation.
- Stable combustion of a small rocket engine by catalyst ignition
- Advanced Onboard Processing of Telemetry and Command (Part I)-System Design-
- Advanced Onboard Processing of Telemetry and Command (Part II)-Prototyping and Evaluation-
- Study of space-borne reconfigurable component
- Design trials of On-board digital equipments by C based system level design tool
- Mission summary and status of Greenhouse gases Observing Satellite (GOSAT)
- Evaluation of the MicroLabSat operation on Orbit
- On-Orbit Evaluation of Residual Magnetic Moment for REIMEI Satellite
- On System and Development of Small, Advanced Scientific Satellite "INDEX"
- Auroral research with Reimei satellite
- On-orbit Performance of the REIMEI Satellite with Integrated Computer System and Flexible Operation
- Design and in-orbit evaluation of REIMEI attitude determination and control system
- On-Orbit Results of REIMEI's Solar Concentrated Paddles with Thin Film Reflector
- In-Orbit Performance of the Lithium-Ion Secondary Battery for 'REIMEI'
- Development and On-Orbit Results of Miniature Space GPS Receiver by means of Automobile-Navigation Technology
- Potential of small satellites for commercial and government applications
- A study on microgravity experiments using excess performance capability of H-IIA
- Microgravity combustion research utilizing new 50m drop tower
- Flight results of micro-gravity experiment system using a high altitude Balloon
- Detection evaluation of geostationary earth orbit debris
- JAXA's Optical Observation Facility for Space Debris
- A discussion about the duration time of microwave emissions accompanying hypervelocity impacts
- Development of Hypervelocity Gun by Pulse Power
- Improvement of Conical Shaped Charge System and comparison of the test results between CSC and gas gun
- Properties of Fragment from Micro Satellite Impact Experiments
- Damage characteristics of composite materials on hypervelocity and low velocity impact
- Design and Conception of i-Ordin(intelligent Orbital debris interceptor)
- Rotational motion estimation of LEO debris
- Rotational motion analysis of LEO debris
- Model-based motion estimation of a failed satellite using imaging
- Development of High Performance Camera System for On-Orbital Satellite Maintenance
- Technology for Extreme Environment - Activities of Laboratory of Spacecraft Environment
- Lessons and Perspective of Space Research Education based on Actual Small Satellite Development Experiences in Tokyo Tech
- Development of Nano-Satellites for Regional Disaster Prevention-Industry-University-Government Collaborated Activities in Kagoshima-
- The Student Rocket of KIT Flies in the French Sky of La Courtine
- Launch Experiment of Open Class CanSats by Japanese Student High Power Rocket
- Hokkaido Satellite Project
- Development and Launch Experiment of 400 kgf Thrust Class CAMUI Hybrid Rocket
- Study on High-performance Non-combustion Small Rocket Engine by using Valveless System
- HTV Evolution Plan
- Concept Studies of HTV Derived Re-entry System
- Commercial ISS Cargo Logistics for NASA using HTV
- Space parcel delivery by HTV
- JEM Utilization Future Plan and HTV Transportation
- Abstract of Microgravity Experiment by Rocket (Part.1)
- a Concept Design of Microgravity Experiments by Rocket (vol.2)
- Limit performance of ball bearings for rocket engine turbopumps
- Simulation Model of Semi-Closed Ecological System for Space Plantation
- Study of Water-Energy-Cycle Space Propulsion System for Flight Readiness
- Preliminary Study of Hydrogen Storage Technology in Space
- Overview of High Accuracy Positioning Experiment System using QZSS
- System Design of Quasi-Zenith Satellite Navigation System
- Development of Apparatuses and Software of RESSOX for QZS Experiments
- Experiments of Remote Synchronization System Using Multiple Positioning Signals for Feedback Control
- RESSOX Validation Experiments Demonstrated with Geostationary Satellite
- Automatic Generation of Procedures for Spacecraft Mission Operations
- Implementation of CCSDS SLE RAF/F-CLTU Services and result of launch operation.
- Experiment of Realtime Broadcasting System for Satellite's Data and Status
- A study of dynamic update flight software for spacecraft
- The current status on Japanese Experiment Module "KIBO" of International Space Station.
- Risk Management in ISS Project - Measures to Prevent Failures using the Analysis Method of "Thread of Connection"
- Risk Management of International Space Station Program(means of extracting risk by Event Sequence FMEA)
- Current Status of SERVIS Project
- COTS Parts Evaluation for SERVIS Project
- On-orbit Operation of SERVIS-1
- Measurement of Space Radiation Environment by EMSS
- Development and Space Experiment Results of Vane Type Propellant Tank System
- Evaluation of Orbital Results from SERVIS-1 INU
- Development of the Power Control and Distribution System, and the result of experiment in space
- Development of Advanced Paddle Drive Mechanism (APDM), and the result of on-orbit experiment
- Development of advanced TTC Transponder and its on-orbit experimental result
- Summary of OICETS Project
- Modification on OICETS for replacement of launch vehicle
- Launch Base Support and Lauch Evaluation of OICETS "Kirari"
- Operation summary of OICETS
- OICETS system on-orbit evaluation results
- On-orbit Performance Evaluation of Attitude and Orbit Control System of Optical Inter-orbit Communications Engineering Test Satellite (OICETS)
- Orbital Performance of OICETS Ni-MH Batteries
- On-orbit test results of OICETS
- Optical communication performance of OICET-ARTEMIS intersatellite link experiments
- Evaluation of emitted laser beam in OICETS-ARTEMIS communication experiments
- Optical performance evaluation of the Laser Utilizing Communications Equipment (LUCE)
- Pointing Control Performance Assessment of Optical Communication Terminal (LUCE)
- Laser Communication Experiments between OICETS and NICT Optical Ground Station
- Operation of the OICETS' Optical Ground Station Experiment
- Error Correction Coding Design for Ground-to-OICETS Laser Communications
- OICETS Mission Planning and Scheduling System
- Evaluation of Optical Inter-satellite Communications Experiment from Operability Perspective
- Research of Powdered Propellant Propulsion for Practical Use on Microsatellites
- The experimental study for accuracy improvement of ultrasonic flowmeter
- Photon Pressure Space Propulsion via Direct Energy Conversion
- Ground Experiments of Current Collection by a Bare-Tether in a High-Speed Flowing and Magnetic Plasma
- Thrust Measurements of Microwave Discharge Hall Thruster
- A Study of Index Parameters of Low Frequency Oscillation in a Hall Thruster
- Plasma and Ion Beam Characteristics of a Hall Thruster with a Circular Cross-sectional Discharge Chamber
- Development Status of Power Processing Unit for 250mN-class Hall Thruster
- Study on Effects of Nonuniformity Mixture Ratio in Injector
- Structural analysis of LE-5B engine combustion chamber
- Experimental Validation of Thrust Performance of Water/Liquid Nitrogen Rocket Engine
- Experiments on N2O/Ethanol Propulsion Systems
- Initial Plasma-Nuclei Formation Processes in Laser-Ignition
- The Effect of Mixture Ratio of B/KNO3 on a Laser Ignition Microthruster Performance
- FUNDAMENTAL STUDY OF LASER-IGNITED MICROTHRUSTERS
- Evaluation of Turbo Decoding System for the Next Generation Deep Space Ground Station
- Experimental Mission of STARS-I by Inter-Satellite Communication
- The control method for "Turn over problem" of the electro dynamic tether satellite system
- Stabilization of Electrodynamic Tethers by Current Control
- Feasibility study on aero-braking combined with Electro-dynamic Tether
- Numerical Simulations on the Tether Deployment including an Attitude Motion of the Mother Satellite
- Experimental Study on Tape Tether Deployment of Sounding Rocket Project
- Analysis of vibration and Control of Tethered Space Solar Power System
- Deployment and Retrieval of Tethered Space Robot for Pico Satellite
- Experimental Study on Manual Operation Method of a Space Robotic Arm Considering Vibration Suppression
- Dexterous Tasks for Experiments Utilizing Space Exposed Environment by Space Robotic Arms
- The image measurement system for structure assemblies in space
- Concept of a Morphable Beam Device and its Application to Spacecraft Inspection
- A strategy to develop the space robot technology for future space missions
- The meal assistance robot using Slant-axis multijoint manipulator
- System Design of HAYABUSA Asteroid Explore
- Powered Flight in Deep Space by Microwave Discharge Ion Engines
- Hayabusa Orbit Determination from the Launch to the Arrival at the Target Asteroid
- Hayabusa Cruise Operation
- Hayabusa Navigation and Guidance in Approach and Proximity Phase
- Observation of Asteroid Itokawa by Multiband Imager of Hayabusa
- Pole and Global Shape of 25143 Itokawa
- Near-Infrared Spectral Observation of Asteroid Itokawa by Near-Infrared Spectrometer onboard Hayabusa Spacecraft
- X-Ray Fluorescence Spectrometry of Asteroid Itokawa by Hayabusa XRS
- Mass and Local Topography Measurements of Asteroid Itokawa by LIDAR aboard Hayabusa
- Results achieved through MINERVA Rover in Hayabusa Mission
- Flight Results on Descent and Touchdown for Asteroid Exploration Spacecraft HAYABUSA
- Development and Operation of the Hayabusa Asteroid Surface Sampling Device and Its Sample Analysis Preparation
- In-Orbit Operation of the Electrical Power Sub-System for 'HAYABUSA'
- Lessons learned from HAYABUSA Attitude and Orbit Control System
- Summary of the current results of Hayabusa mission and the future plan
- Welding Experiments by Diode Laser Welding at Space Station Orbital Pressure
- Welding Experiments of Aluminum Pipes by Space GHTA Welding Process under Simulated Space Environment.
- The study of solder joint for parts
- Molecular Contamination Analysis on SOLAR-B/OTA
- Experimental approach for photocatalytic decontamination under vacuum conditions
- Development of Atomic Oxygen Concentrator (4)
- Properties of Outgas and Mechanical Properties on Lightweight Sandwich Panel
- Discoloration of Polyimide after Irradiation
- Interaction between effect of complex environment in low earth orbit and spacecraft polymeric materials
- An Evaluation of Endurance of Grese-lubricated Elctric Contact with MAC Grease
- Making and Testing of a Hot Gas Generator for Evaluation of C/C Composite Cooling Structure.
- Electrical power subsystem design of machine micro satellite "HITSAT" of M-V-7 Subpayload
- Influence of Catalyst Composition on Performance of Polymer Electrolyte Fuel Cell
- Study of Electric Double Layer Capacitors for Long-Life Electrical Power Sub-Systems
- Electrical Breakdown Tests on Space Insulating Materials for Spacecraft Design Criteria
- WINDS Program
- Overview of Satellite Communications System for WINDS
- The developments of Ka band multi-beam antenna for WINDS
- Ka band High Power Multi-port Amplifier (MPA) for WINDS Satellite
- Development of Active Phased Array Antenna for WINDS
- Development of Active Phased Array Antenna control systems for WINDS
- Development of On-board Baseband Switch for WINDS
- Coverage Analysis of WINDS Communication Links
- Development of WINDS Experiment Ground Station System
- The Development of the High-Speed Network for the WINDS
- Network Control of the WINDS Communications System
- A compensation control for downlink rain attenuation in WINDS and simulation results
- Approach for commercialization of the satellite and on-board equipment
- GX Launch Vehicle: A Case Study of Space Technology Commercial Application
- Commercial Launch Services of the H-IIA Rocket
- Japanese-made Manned Space Ship Development Vision by Civil
- Civil Commercial Astronaut "Mission Commander" and New Vision of Civil Space Business
- A study of electrode fall voltage in an MPD thruster
- Nozzle Geometry Optimization of Quasi-One-Dimensional MPD Thruster Considering Pressure Gradient
- Study on Optimization of Nozzle and Discharge Room Configurations of Electrothermal Pulsed Plasma Thrusters
- Evaluation of Effects of Nozzle Attachment and Cathode Dimension on Coaxial-PPT Performances
- The design, production and performance test of a pulsed plasma thruster as a space education
- Fundamental Study of Micro-Arcjet Array Thrusters
- Research and Development of Microwave Discharge Ion Engine .MU.20
- Optimization of Antenna Configurations for Microwave Discharge Ion Engines
- Expansion of Brophy Model to Microwave Discharge ECR Ion Source
- Fourfold Double Sheath Model of a Neutralizer Hollow Cathode
- An Endurance Test of a Hollow Cathode for the Next-Generation Ion Engine
- Dependence of Magnetic Field Configuration on Thrust Performance in Miniature Ion Thruster
- Fundamental study of Laser Accelerated Plasma Thruster
- Fundamental Study for Operating Characteristics of LASER-Electric Hybrid Propulsion
- Numerical simulation of fusion plasma behaviors in a magnetic nozzle for laser fusion rocket
- Study on Flow Field and Magnetic Field around Magneto Plasma Sail
- Construction of high density plasma by helicon source
- Utilization of launcher for small rocket launch in Akita
- Student space development activity in Noshiro
- Space Development Projects for Scientific Missions at Tohoku University-Stratosphere Balloon, Sounding Rocket, and Micro Satellite
- Mission analysis for Kyushu small satellites (Hyperspectral radiometer)
- Development of nano-satellite for Tokyo Metropolitan College of Aeronautical Engineering
- Space Development in Soka University
- Boom for Micro-satellite "SOHLA-1": Development of Prototype Model
- The Student Participation in the Micro Satellite "SOHLA-1" Development and the Role of the "Small Spacecraft Systems Research Center"
- Kagawa Satellite Development Project and Its Community
- Space Development and Business Activity in Hokkaido
- "The Manten Project" Status and Issues for production on Aerospace Industry
- A New Aerospace Industry in Cooperation with Local Industries and their Technologies
- Microsatellite development by small and medium-sized enterprises
- The present situation of development of space technology in Kyushu region
- Improvement of tele-controll precision for exploration Rover by target tracking using Mean-shift
- Performance Evaluation by Monte Carlo Method of Remote Control Method that Used Command Path Compensation
- Accuracy evaluation of Global Map Generation Method by Iterating Overlap-part Estimation
- A Study of Observation system in the Lunar Surface Low Frequency Radio Wave Observatory.
- Feasibility Assessment of Venus Balloon Mission
- Modeling and Dynamics of the Planetary Airship System(PLAS) on Venus
- Geostationary Satellite System with only Solar Electric Propulsion (1)-Orbital Transfer Analysis-
- Geostationary satellite system with only solar electric propulsion (2)-Satellite system configuration-
- Orbit Determination with Two-way Satellite Time Transfer Data
- A Study on the Orbits for Gravitational Wave Antenna DECIGO
- Possible observation instruments for precise orbit determination of ASTRO-G satellite
- Solar radiation pressure model of ASTRO-G satellite
- Evaluation of Delta-VLBI with HAYABUSA at Touchdown to Itokawa
- Mass Estimation of Asteroid Itokawa by using Range, Doppler and ONC Data
- Status of Trajectory Planning of Next Asteroid Explorer Mission
- Development Status toward the final version of Multi-Utility Spacecraft Charging Analysis Tool (MUSCAT)
- 3D Spacecraft Modeling by Using GUI of MUSCAT (Multi-Utility Spacecraft Charging Analysis Tool)
- Temperature influence on charge accumulation inside dielectric films
- Measurement of sustained arc threshold for satellite solar arrays
- Overview of Studies on Space Solar Power Systems of JAXA
- Study of Technology Demonstration Mission in SSPS
- Overview of the USEF SSPS Activities
- SPS Related Research at AIST
- Mitigation Methods of discharge on Satellite Solar Array in Geosynchronous Earth Orbit Environment: Experimental Study
- Discharge phenomena on a solar array under microwave irradiation
- Degradation of Solar Cell Due to Electrical Discharge in Plasma Environment
- Influence of Array Potential Distribution on Plasma Interaction with High Voltage Solar Array
- Opinion poll to SSPS
- Laser energy transmission for an Unmanned Airplane
- Results of Recent ITU-R Activities toward Frequency Allocation for SSPS-Extension of the completion date of Question ITU-R 210/1-
- Microwave Beam Control for SSPS
- GaN microwave power device for Space Solar Power System
- Flight Characteristics of Kindai Pet-bottle Rocket
- PIV analysis of Opposing Jet Flow Field around Vertical Landing Rocket Vehicle
- Consideration of Autonomous Control System Small Movable Wing for CAMUI Hybrid Rocket
- CFD Design Study of Aerodynamic Characteristics of Lifting Body Flight Experiment (LIFLEX) Vehicle for Combined Control Surface Efficiency at Subsonic Landing Phase
- Feasibility Study on the Magnetic Flow Control for a Reentry Vehicle
- Control of Aerodynamic Characteristics for a Reentry Vehicle by Using Electromagnetic Force
- A Study of the Reentry Survivability Analysis
- Quantification of Effect to Shock Wave by Precursor Heating
- Numerical Analysis of Reduction of Aerodynamic Heating by Electro-Magnetic Force
- Feasibility of Electromagnetic Heat Shield in a Hypersonic Flight and Its Application to Space Plane
- Supersonic Drag Reduction by pulsed-laser plasma
- Effect of the Surface Catalycity on the Flight Performance of the Injection Cooling Method for a Reentry Vehicle
- Pyrotechnics Developments of Recovery System for NEXST-1
- Development of Parafoil Deployment Mechanism for Small Experimental Rocket Recovery
- Evalution of Flight Characteristics of Recovery Parafoil by Free Flight Experiments
- The automatic-flight experiment of small-size parafoil for improvement in guidance performance
- A study on water-impact shock of reentry capsule
- Critical Design of On-board Time Transfer Subsystem for quasi-zenith satellite system
- Interface Design for the Time Management System for Satellite Positioning System using Quasi-zenith Satellite
- Operation of time management system for a quasi-zenith satellite system (QZSS)
- Transmission suspension operation of time comparison link in QZSS
- Master Control Station for High Accuracy Positioning Experiment System
- Interface Specification for Quasi-Zenith Satellite System (QZSS)
- Long term variation of quasi-zenith satellite orbit in case of minimum station keeping
- Interference Estimation toward the FS Communication Systems Generated by the NGSO Communication Systems
- Aroused a motivation to develop Ku-band tracking system by a beacon signal from Quasi Zenith Satellite
- Development of Pseudo Quasi-Zenith Satellite and Flight Experiment
- Development and Evaluation of Off-line High-accuracy Positioning Test System
- Mitigation for GBAS Integrity Risk using Satellite Monitor
- Tropospheric Delay Correction of GPS Signals for Sub-meter Class Positioning
- Prototype Evaluation of QZSS Submeter-Class Wide-Area Differential Corrections
- Improvements on Ionospheric Parameters Optimized by Regional Limitation
- Improvement of Positioning Accuracy utilizing Modernized Positioning Signals
- The Evolutional concept to the Regional Satellite Navigation System from Quasi-Zenith Satellite System (QZSS)
- Development of On Board Computer and Result of Space Verification, SERVIS-1 Experimental Component
- Development and Flight Results of SIS (Satellite Controller Integrated with Star Sensors)
- Development and Results of Space Experiment for Lithium-Ion Battery System
- Development and Demonstration of Fiber-Optic Gyro-Inertial Reference Unit
- Development of SERVIS-2-Space Environment Reliability Verification Integrated System Spacecraft-2-
- Development of a Lithium Ion Battery System with Automotive Technology (LIBA)
- Development of a High Assurance Data Management System (ADMS) for Use on Space Systems
- Development of the Autonomous Fault Tolerant Computer System
- Development of the Remote Terminal Experiment Equipment
- Development of High Performance Data Compressor, SERVIS-2 Experimental Component
- Development of APE-Advanced Positioning Experiment System-
- Development of Advanced Satellite Structure Experimental Module
- Development of Magnetic Bearing Wheel
- Current Sensorless Power-Amplifier for Magnetic Bearing Wheel
- Development of the test equipment for RF-MEMS
- A Study on MEMS Equipment for Space Application
- Radiation verification test result of GaN FET for next generation space use SSPA
- The Design of Spin Axis Control System of Micro Satellite "SOHLA-1"
- Development of Attitude Sensors of Small Satellite
- Application of Inflatable Actuated Ultra-Light Extendible Member
- Attitude Control for Efficient Improvement of Space Solar Power Satellite
- Flight Test of Rocket Sun Aspect Sensor and Attitude Determination System on the Ground by M-V-8 Launch
- The comparison of membrane shape of Solar Sail in numeric analysis
- Evaluation of Pointing Error for SOLAR-B Using Optical Measurement
- Inflight Data of CCD Star Tracker for Attitude Determination and Control of AKARI
- Vibration modes in the equilibrium of a rotating circular solar sail membrane
- Development Of high reliability-Inertial Reference Unit
- A consideration about membrane deployment dynamics of tether controlled solar sail
- Micro Gravity Experiment of Angular Velocity Stabilization using Variable Speed Control Moment Gyro
- Tiny GPS Receiver with Onboard Navigation Capability
- Study on Light Curable Space Inflatable Structures Technology by Triaxial Woven Fabric
- Singularity Avoidance of Control Moment Gyroscopes using optimization of initial gimbal angles for satellite attitude control
- Accuracy Evaluation on Altitude Measurement of the Landing Radar based on Field Experiments
- A Study on the Folding Characteristics of Triaxially Woven Fabric Composite Structures
- Inner Disturbance Accommodation Filter of Control Moment Gyros with Adaptive Observer
- Experiment of Microwave Beam Control using a S-310-36 Sounding Rocket
- Surface Error Estimation of A Membrane Reflector Constructed with High-Accuracy Gore Membrane
- Disturbance Isolation Platform Design Method for Reaction Wheel for Control Satellite Attitude
- Development of Moving Mechanical Components for Space-Use
- Deployment Experiments of Deformation-free Simplified Inflatable Polygons
- System Study on the Next Generation Star Tracker
- Development of High Gain Antenna (HGA) for Mercury Magnetospheric Orbiter (MMO)
- A Study on dynamic Behavior of Ultra-lightweight Extendible Space Structure Spinning around its axe using an idealized simple model.
- Study and Evaluation of High Performance Fiber Optic Gyro Inertial Reference Unit
- The Study of Influences of Modifications for Flight Model on Middle Gain Antenna of Mercury Magnetospheric Orbiter
- Effects of Structural Properties on Deployment/Retraction characteristics of Retractable Inflatable Tubes
- Development of a New Generation Spaceborne GPS Receiver
- Wide-Temperature Test of Fluxgate Magnetometer Sensor for Mercury Exploration
- Application of a multi-cellular inflatable structure to large space systems
- Study and Development on advanced reaction wheels with high performance
- Characteristics of a Trial-fabrication Transparent MEMS Lightwave Antenna for a Wire-less Communication
- Conceptual Tensegritiy Models with Multi-cellular Inflatable Tubes
- Study on the Navigation Laser Sensor for Spacecraft Rendezvous Missions
- Development of the prediction system for random vibration of satellite equipment panel subjected to acoustic excitaion
- In-Orbit Test of Thick Film Type Variable Emittance Radiator
- Precise Attitude Control Experiment and Control System Design of ETS-VIII
- A study on higher-order spectral techniques for detection of mechanical vibrations
- A Brief Note on numerical method of dynamics of membrane structure
- On-Orbit System Identification Experiment of ETS-VIII
- Experimental Study on Vibration Control of Space Solar Power Satellite
- Synchronous Deployment of Solar Array using Parameter Control
- System Identification Using Impulse Response Including Initial States
- Prediction of Pyroshock Response of the Spacecraft Interface Induced by V-band Clamp Separation Devices with Circular Ring Model
- Introduction of research of high agility maneuver for artificial satellite in JAXA IAT
- Development of Spin Ejection Device for MMO
- A Design Method for Cablenetworks Considering Supporting Structures
- Integration of Attitude Control System and Image Processing System for Observation Satellite
- Rib Design of Mesh Reflector
