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Extending the ECOB space debris index with fragmentation risk estimation

Extending the ECOB space debris index with fragmentation risk estimation
Extending the ECOB space debris index with fragmentation risk estimation
In recent years several formulations of debris indices have been proposed to provide a fast assessment of the criticality of a space object in terms of its impact on the debris environment. In a previous work, we proposed a formulation (ECOB, Environmental Consequences of Orbital Breakups) based on the evaluation of the consequences of the fragmentation of the studied object in terms of the increase in the collision probability for operational satellites. This work discusses the extension
of that approach by considering not only the effect of the fragmentation but also its likelihood. In addition, a method to take into account different End-of-Life scenarios and the application to constellations are discussed.
European Space Agency
Letizia, Francesca
2cd64b5f-c294-4856-9c50-ad002c25bb31
Colombo, Camilla
595ced96-9494-40f2-9763-ad4a0f96bc86
Lewis, Hugh
e9048cd8-c188-49cb-8e2a-45f6b316336a
Krag, Holger
6d775d65-8e5a-4053-a4e7-16c9cf32a7cf
Letizia, Francesca
2cd64b5f-c294-4856-9c50-ad002c25bb31
Colombo, Camilla
595ced96-9494-40f2-9763-ad4a0f96bc86
Lewis, Hugh
e9048cd8-c188-49cb-8e2a-45f6b316336a
Krag, Holger
6d775d65-8e5a-4053-a4e7-16c9cf32a7cf

Letizia, Francesca, Colombo, Camilla, Lewis, Hugh and Krag, Holger (2017) Extending the ECOB space debris index with fragmentation risk estimation. In 7th European Conference on Space Debris: 17 April 2017 - 21 April 2017, Darmstadt, Germany. European Space Agency..

Record type: Conference or Workshop Item (Paper)

Abstract

In recent years several formulations of debris indices have been proposed to provide a fast assessment of the criticality of a space object in terms of its impact on the debris environment. In a previous work, we proposed a formulation (ECOB, Environmental Consequences of Orbital Breakups) based on the evaluation of the consequences of the fragmentation of the studied object in terms of the increase in the collision probability for operational satellites. This work discusses the extension
of that approach by considering not only the effect of the fragmentation but also its likelihood. In addition, a method to take into account different End-of-Life scenarios and the application to constellations are discussed.

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Letizia_ECOB_extension - Accepted Manuscript
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More information

Accepted/In Press date: 15 December 2016
Published date: 18 April 2017
Additional Information: Related publications: Colombo, C. et al (2017). Life cycle assessment indicator for space debris. Paper presented at 7th Space Debris Conference, Darmstadt, Germany. Letizia, F. et al (2016). Assessment of breakup severity on operational satellites. Advances in Space Research, 1-57. Letizia, F. et al (2017). Development of a debris index. In Stardust Final Conference - Advances in Asteroids and Space Debris Engineering and Science. Springer.
Venue - Dates: 7th European Conference on Space Debris, , Darmstadt, Germany, 2017-04-18 - 2017-04-21
Organisations: Aeronautics, Astronautics & Comp. Eng, Astronautics Group

Identifiers

Local EPrints ID: 411725
URI: http://eprints.soton.ac.uk/id/eprint/411725
PURE UUID: 8a3be9ec-cd0a-450f-af9f-27d4aee98269
ORCID for Francesca Letizia: ORCID iD orcid.org/0000-0002-2877-8012
ORCID for Camilla Colombo: ORCID iD orcid.org/0000-0001-9636-9360
ORCID for Hugh Lewis: ORCID iD orcid.org/0000-0002-3946-8757

Catalogue record

Date deposited: 22 Jun 2017 16:31
Last modified: 16 Mar 2024 02:55

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Contributors

Author: Francesca Letizia ORCID iD
Author: Camilla Colombo ORCID iD
Author: Hugh Lewis ORCID iD
Author: Holger Krag

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