On the Usages and Functions of Particles -kou_/-ka. in Colloquial Burmese
Flight status of IKAROS deep space solar sail demonstrator
Flight status of IKAROS deep space solar sail demonstrator
Development of a Magnetic Suspension and Balance System for Supersonic Wind Tunnels (AIAA 2014-1312)
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]
IKAROS, a Solar Sail Demonstrator and Its Application to Trojan Asteroid Exploration
Input Shaping Experiment for Damping Vibration in Manual Operation of a Large Robotic Arm
A Spin-up Control Scheme for Contingency Deployment of the Sailcraft IKAROS
Model experiment on parametric rolling of a post-panamax container ship in head waves
Feasibility of Magnetic Suspension and Balance System as On-Ground Test Facility of Space Structures
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