Sensitivity analysis of launch activities in Low Earth Orbit
Sensitivity analysis of launch activities in Low Earth Orbit
This work aims to investigate the response of the low Earth orbit environment to the change in number and distribution of new launches and to understand the effects of the size and post-mission lifetime of a large constellation of spacecraft. The analysis presented in this paper were carried out using MISSD, Model for Investigating control Strategies for Space Debris, a multi-shell, and multi-species source-sink statistical model able to simulate the injection, removal and interaction of six type of objects up to an altitude of 2000 km. The results suggest that multiple regions experience a sensible increment in the orbital density when slightly increasing the launch activity for the next 200 years. Recently, many private companies expressed their interest in putting large constellations of satellites at 1100–1300 km altitude. However, results show that the launch of just six additional spacecraft per year in this region increased the spatial density by an amount equal to the projection over 200 years of today's most crowded region. Results also show that the increase in the orbital population and collision risk caused by the presence of large constellations could be mitigated using a high level of post-mission disposal compliance, reliable deorbit mechanisms and reducing thepost-mission lifetime to 5 years.
space debris, low Earth orbit, sensitivity analysis, satellite constellations, space sustainability
Somma, Gian Luigi
fe2f9516-1fdb-4b9b-a4ce-7b6a7e60b49a
Lewis, Hugh G.
e9048cd8-c188-49cb-8e2a-45f6b316336a
Colombo, Camilla
595ced96-9494-40f2-9763-ad4a0f96bc86
Somma, Gian Luigi
fe2f9516-1fdb-4b9b-a4ce-7b6a7e60b49a
Lewis, Hugh G.
e9048cd8-c188-49cb-8e2a-45f6b316336a
Colombo, Camilla
595ced96-9494-40f2-9763-ad4a0f96bc86
Somma, Gian Luigi, Lewis, Hugh G. and Colombo, Camilla
(2018)
Sensitivity analysis of launch activities in Low Earth Orbit.
Acta Astronautica.
(doi:10.1016/j.actaastro.2018.05.043).
Abstract
This work aims to investigate the response of the low Earth orbit environment to the change in number and distribution of new launches and to understand the effects of the size and post-mission lifetime of a large constellation of spacecraft. The analysis presented in this paper were carried out using MISSD, Model for Investigating control Strategies for Space Debris, a multi-shell, and multi-species source-sink statistical model able to simulate the injection, removal and interaction of six type of objects up to an altitude of 2000 km. The results suggest that multiple regions experience a sensible increment in the orbital density when slightly increasing the launch activity for the next 200 years. Recently, many private companies expressed their interest in putting large constellations of satellites at 1100–1300 km altitude. However, results show that the launch of just six additional spacecraft per year in this region increased the spatial density by an amount equal to the projection over 200 years of today's most crowded region. Results also show that the increase in the orbital population and collision risk caused by the presence of large constellations could be mitigated using a high level of post-mission disposal compliance, reliable deorbit mechanisms and reducing thepost-mission lifetime to 5 years.
Text
Somma_2018_Sensitivity_Analysis_of_Launch_Activities_in_Low_Earth_Orbit
- Accepted Manuscript
More information
Accepted/In Press date: 21 May 2018
e-pub ahead of print date: 31 May 2018
Additional Information:
Invited article for a special issue of Acta Astronautica
Keywords:
space debris, low Earth orbit, sensitivity analysis, satellite constellations, space sustainability
Identifiers
Local EPrints ID: 422558
URI: http://eprints.soton.ac.uk/id/eprint/422558
ISSN: 0094-5765
PURE UUID: f0f0cac4-3896-4309-b258-545341098f56
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Date deposited: 25 Jul 2018 16:30
Last modified: 16 Mar 2024 06:54
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Contributors
Author:
Gian Luigi Somma
Author:
Camilla Colombo
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