Simulation and modelling of orbital debris environment by equivalent breakups

Advances in Space Research

Volumn 19, Issue 2, 1997, Pages 309-312

  Ganeshan, A S ^a   Ananthasayanam, M R ^b  

^a INDIAN SPACE RESEARCH ORGANISATION   (India)

^b INDIAN INSTITUTE OF SCIENCE   (India)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; EXPLOSIONS; MATHEMATICAL MODELS; ORBITS; RISK ASSESSMENT; SPACE STATIONS; SPACECRAFT; TRACKING (POSITION);

COLLISION PROBABILITY;

SPACE DEBRIS;

EID: 0030649326     PISSN: 02731177     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0273-1177(97)00019-7     Document Type: Article

References (4)

1. Badhwar, G.D., and P.D. Anz-Meador, Determination of the Area and Mass Distribution of Orbital Debris Fragments, Earth, Moon and Planets, No.45, pp 29-51 (1989).
2. Ganeshan, A.S., S.C. Rathnakara, S. Banerjee, Modelling the low Earth Space Debris Environment, Journal of Spacecraft Technology, Vol. 4, No.2, pp. 52-59 (1994)
3. Sdunnus, H., Comparison of Breakup Models,Proceedings of the 13th Inter-Agency Space Debris Coordination Meeting, Darmstadt, Germany (1996).
4. Su, S.-Y and D.J. Kessler, Contribution of Explosions and Future Collisions Fragments to the Orbital Debris Environment,Advances in Space Research, Vol 5, No.2, pp 25-34 (1985).