On the Usages and Functions of Particles -kou_/-ka. in Colloquial Burmese
Development of a Magnetic Suspension and Balance System for Supersonic Wind Tunnels (AIAA 2014-1312)
Flight status of IKAROS deep space solar sail demonstrator
Flight status of IKAROS deep space solar sail demonstrator
The Effect on Traffic Flow During Total Road Closures Due to Road Repairs
Evaluation of the weather criterion by experiments and its effect to the design of a RoPax ferry
Brillouin nonlinearity as a mechanism of dynamic holography [4353-38]
A Spin-up Control Scheme for Contingency Deployment of the Sailcraft IKAROS
IKAROS, a Solar Sail Demonstrator and Its Application to Trojan Asteroid Exploration
Feasibility of Magnetic Suspension and Balance System as On-Ground Test Facility of Space Structures
Model experiment on parametric rolling of a post-panamax container ship in head waves
Input Shaping Experiment for Damping Vibration in Manual Operation of a Large Robotic Arm
A Study on Membrane Deformation of Solar Power Sail Demonstrator IKAROS
Shape Estimation of IKAROS's Solar Power Sail by Images of Monitor Cameras
Trajectory Reconstruction of the Ikaros DCAM2 (AAS 11-246)
Titech ARLISS Project 2001 and Autonomous Flying Experiment
Mission Report on The Solar Power Sail Deployment Demonstration of IKAROS
Development of laser turning using femtosecond laser ablation [4426-63]
Micro-machining using 1.55mum band fiber pulse laser with 10kW peak power [5662-82]
Tree Height Estimation by Airborne Interferometric SAR
Analysis of Membrane Dynamics using Multi-Particle Model for Solar Sail Demonstrator ``IKAROS''
AIAA-2003-2388 Tokyo Tech CubeSat: CUTE-I - Design & Development of Flight Model and Future Plan
Titech CanSat Project 2000: Report of Sub-orbital Flight and Balloon Experiment
Tokyo Tech 1kg Pico-Satellite CUTE-1 - Development, Launch & Operations
Titech CanSat Project 2000: Report of Sub-orbital Flight and Balloon Experiment
Repeatability of Stored Configuration of a Large Solar Sail with Non-negligible Thickness
Titech Micro-Satellite Model: CanSat for Sub-Orbital Flight
High-Performance Image Acquisition & Processing Unit Fabricated using COTS Technologies