A model of distribution of geostationary satellite fragments after explosion

Details A model of distribution of geostationary satellite fragments after explosion A model of distribution of geostationary satellite fragments after explosion

Oct 2001

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2001esasp.473..407v&link_type=abstract

In: Proceedings of the Third European Conference on Space Debris, 19 - 21 March 2001, Darmstadt, Germany. Ed.: Huguette Sawaya-L

Physics

Space Debris, Distribution, Satellite Breakup

Scientific paper

The influence of the velocity changes ΔV originated after a satellite explosion, on initial orbits of satellite fragments have been examined. These orbits have been expressed through orbital element of parent body and ΔV. The obtained formulas have been tested with the use of observable fragments of satellite 77092A (Ekran 2). Taking into account the orbital evolution of fragments it has been shown that the volume of the region of their distribution is significantly larger than the volume of the geostationary ring where the all observable objects move.

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