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Longitude-dependent effects of fragmentation events in the geosynchronous orbit regime
Institution:1. Department of Aerospace Science and Technology, Politecnico di Milano, Milano, Italy;2. IFAC-CNR, Sesto Fiorentino, Italy;3. Advanced Space Concepts Laboratory, University of Strathclyde, Glasgow, UK;4. Astronautic Research Group, University of Southampton, Southampton, UK;5. ESA/ESOC, Darmstadt, Germany;1. IFAC-CNR, Via Madonna del Piano 10, 50019 Sesto Fiorentino, Italy;2. IAPS-INAF, via Fosso del Cavaliere 100, 00133 Roma, Italy
Abstract:The effects of on-orbit fragmentation events on localized debris congestion in each of the longitude slots of the geosynchronous orbit (GEO) regime are evaluated by simulating explosions and collisions of uncontrolled rocket bodies in multiple orbit configurations, including libration about one or both of the gravitational wells located at 75°E and 105°W. Fragmentation distributions are generated with the NASA Standard Breakup Model, which samples fragment area-to-mass ratio and delta-velocity as a function of effective diameter. Simulation results indicate that the long-term severity and consequence of a GEO fragmentation event is strongly dependent upon parent body longitude at the epoch of fragmentation, which can spawn bi-annual “fragment storms” in high-risk longitude slots, driven by lower-energy fragments that have been captured and have started librating around the nearby gravitational well.
Keywords:Geosynchronous orbit  Orbital debris  Fragmentation events
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