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Self-induced collision hazard in high and moderate inclination satellite constellations

Self-induced collision hazard in high and moderate inclination satellite constellations
Self-induced collision hazard in high and moderate inclination satellite constellations
The assessment of the hazard posed by space debris to constellations of satellites in low Earth orbit is of growing importance, with the proliferation of proposed and implemented constellation systems with a variety of mission objectives. This applies to current constellation-based commercial communication systems, in particular, since these are typically deployed at altitudes where there is a peak in the space debris environment. An impact risk analysis is performed over a period of up to 1 month after a breakup event using two examples of constellation configurations. The first is similar to the IRIDIUM system, containing around 70 satellites in near-polar orbits at approximately 800 km altitude, and the second is a Globalstar-like configuration with 56 satellites at around 1400 km altitude, distributed in orbit planes inclined at 52°. The analysis is performed using the SDS software, which applies the probabilistic continuum dynamics technique. This has the benefit of being a self-contained and rigorous method. However, it is found to be not well-suited to ‘long-term’ analysis, due to the computational effort required. The risk analysis for the chosen examples is presented, as well as an investigation of the robustness of the method when applied to complex and ‘long-period’ simulations.
0094-5765
191-201
Swinerd, Graham
4aa174ec-d08c-4972-9986-966e17e072a0
Lewis, Hugh
e9048cd8-c188-49cb-8e2a-45f6b316336a
Williams, Neil
c550ad82-7658-4cff-96c5-bb6878d30c46
Martin, Clare
8be490b5-498c-465e-8654-073baf1c3040
Swinerd, Graham
4aa174ec-d08c-4972-9986-966e17e072a0
Lewis, Hugh
e9048cd8-c188-49cb-8e2a-45f6b316336a
Williams, Neil
c550ad82-7658-4cff-96c5-bb6878d30c46
Martin, Clare
8be490b5-498c-465e-8654-073baf1c3040

Swinerd, Graham, Lewis, Hugh, Williams, Neil and Martin, Clare (2004) Self-induced collision hazard in high and moderate inclination satellite constellations. Acta Astronautica, 54 (3), 191-201. (doi:10.1016/S0094-5765(02)00290-4).

Record type: Article

Abstract

The assessment of the hazard posed by space debris to constellations of satellites in low Earth orbit is of growing importance, with the proliferation of proposed and implemented constellation systems with a variety of mission objectives. This applies to current constellation-based commercial communication systems, in particular, since these are typically deployed at altitudes where there is a peak in the space debris environment. An impact risk analysis is performed over a period of up to 1 month after a breakup event using two examples of constellation configurations. The first is similar to the IRIDIUM system, containing around 70 satellites in near-polar orbits at approximately 800 km altitude, and the second is a Globalstar-like configuration with 56 satellites at around 1400 km altitude, distributed in orbit planes inclined at 52°. The analysis is performed using the SDS software, which applies the probabilistic continuum dynamics technique. This has the benefit of being a self-contained and rigorous method. However, it is found to be not well-suited to ‘long-term’ analysis, due to the computational effort required. The risk analysis for the chosen examples is presented, as well as an investigation of the robustness of the method when applied to complex and ‘long-period’ simulations.

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Published date: 2004

Identifiers

Local EPrints ID: 22384
URI: http://eprints.soton.ac.uk/id/eprint/22384
ISSN: 0094-5765
PURE UUID: 563dc7ef-f2d0-4bde-8c76-5ab5600855bb
ORCID for Hugh Lewis: ORCID iD orcid.org/0000-0002-3946-8757

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Date deposited: 20 Mar 2006
Last modified: 16 Mar 2024 02:55

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Contributors

Author: Graham Swinerd
Author: Hugh Lewis ORCID iD
Author: Neil Williams
Author: Clare Martin

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