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Modeling of Collision Flux for the Current Space Debris Environment

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Space Debris

Part of the book series: Springer Praxis Books ((ASTROENG))

Abstract

The terrestrial space environment of intact objects and space debris was characterized in Chapters 2 and 3 for particle diameters ranging from 1 µm to catalog sizes. The collision flux resulting from this environment for an object of a certain size on a given target orbit will be determined in the present chapter.

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4.4 References

  • Bendisch, J., Bunte, K., Sdunnus, H., Wegener, P., Walker, R., and Wiedemann, C. (2002). Upgrade of ESA’s MASTER Model. Technical Report (final report) ESA contract 14710/00/D/HK, ILR/TUBS, Braunschweig.

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  • Klinkrad, H. (1993). Collision Risk Analysis for Low Earth Orbits. Advances in Space Research, vol.13:551–557.

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  • Klinkrad, H. et al. (2003). ESA Space Debris Mitigation Handbook. ESA/ESOC, second edition. issue 1.0.

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© 2006 Praxis Publishing Ltd, Chichester, UK

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Klinkrad, H., Wegener, P., Bendisch, J., Bunte, K. (2006). Modeling of Collision Flux for the Current Space Debris Environment. In: Space Debris. Springer Praxis Books. Springer, Berlin, Heidelberg . https://doi.org/10.1007/3-540-37674-7_4

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  • DOI: https://doi.org/10.1007/3-540-37674-7_4

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-25448-5

  • Online ISBN: 978-3-540-37674-3

  • eBook Packages: EngineeringEngineering (R0)

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