IDEA - The Project for In-Situ Debris Environmental Awareness
Shape Distribution of Fragments from Microsatellite Impact Tests
Orbit Determination of ETS-8 by Pegasus Observatory in Kyushu University (AAS 13-850)
A Search for Possible Breakup Fragments in the Geostationary Region
Low Velocity Impact Test and its Implications to Object Accumulation Model in GEO
Orbital Anomaly Analysis to Detect Breakups in GEO (AAS 14-326)
Understanding Orbit Perturbations to Devise Debris Search Strategies in GEO
Development of Orbital Debris Environment Model in the Low Earth Orbit (AAS 03-453)
Ground-Calibration Tests for Optical Surface Inspection in Space (AAS 03-459)
Micro-Satellite Impact Tests to Investigate Multi-Layer Insulation Fragments
Payload Propulsion Using a Spinning Platform through Tether
Using Breakup Models and Propagators to Devise Debris Search Strategies in GEO (AAS 01-549)
Using Breakup Models and Propagators to Devise Debris Search Strategies in GEO (AAS 01-549)
Near Earth Orbit Debris Identification to Secure Future Earth-Moon Trajectory Mission (AAS 14-320)
GEO Debris Accumulation Model Viewed from Low Speed Impact Tests
Preliminary Simulation for Light Curves of Rocket Body In LEO (AAS 13-323)
Development of an Onboard Inspection Device for Debris Impact on Geosynchronous Satellites