rootbrowseIAC-19A6session 55. Post Mission Disposal and Space Debris Removal (1)Papers1. The in-orbit technologies demonstrations of the RemoveDebris mission2. The ELSA-d End-of-life Debris Removal Mission: Preparing for Launch3. Demonstration of Space Debris Deorbit by Electrodynamic Tether4. Wholesale LEO Debris Capture and Removal Using EDDE5. Simulation and Tension Control of a Tether-Actuated Closing Mechanism for Net-Based Capture of Space Debris6. feasibility analysis of large-size space debris de-orbiting from near-earth orbits with respect to the initial mass of a fuelled sc-collector7. Rapid Computation of MEO Satellite Deorbit Times Using Doubly-Averaged Dynamics8. A Permanent Solution for Controlling the Small Space Debris Population9. Implementation of a high thrust mono-propellant engine on a propulsion module10. Grasping Mechanism concepts oriented to Debris for Removal application. Assisted natural reentry for LEO satellites: impacts on mission and satellite design. Capture of debris in GEO by a heavy collector and towing it to graveyard orbit. The Preliminary Analysis of the Re-entry Orbits of Beidou Inclined Geosynchronous Satellites