Collision Risk Mitigation in Geostationary Orbit

@article{Anselmo2000CollisionRM,
  title={Collision Risk Mitigation in Geostationary Orbit},
  author={L. Anselmo and C. Pardini},
  journal={Space Debris},
  year={2000},
  volume={2},
  pages={67-82}
}
The short- and long-term effects of spacecraft explosions, as a function of the end-of-life re-orbit altitude above the geostationary orbit (GEO), were analyzed in terms of their additional contribution to the debris flux in the GEO ring. The simulated debris clouds were propagated for 72 yrs, taking into account all the relevant orbital perturbations.The results obtained show that 6–7 additional explosions in GEO would be sufficient, in the long term, to double the current collision risk with… Expand
View on Springer
12 Citations
Highly Influential Citations
2
Background Citations
4
Results Citations
1

12 Citations

Citation Type

Citation Type

Space debris mitigation in geosynchronous orbit
  • 22
The long-term interaction of the Italian satellites abandoned in GEO with the orbital debris environment☆
Close approach analysis in the geosynchronous region using optical measurements
  • 10
Orbital Perturbations Due to Massive Rings
  • 13
  • Highly Influenced
  • PDF
Utilization of Residual Helium to Extend Satellite Lifetimes and Mitigate Space Debris
  • 1
  • Highly Influenced
  • PDF
Maneuver Estimation Model for Geostationary Orbit Determination
  • 4
Global Risks and Threats to Humanity from Outer Space: Prospects of Warning and Parrying
Parallel Computation of Trajectories Using Graphics Processing Units and Interpolated Gravity Models
  • 31
Robust optimization of impulsive orbit transfers under actuation uncertainties
  • 5
Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime
  • 1
...
1
2
...