The number of artificial objects in orbit continues to increase and, with it, a key threat to space sustainability. In response, space agencies have identified a set of mitigation guidelines aimed at enabling space users to reduce the generation of space debris by, for example, limiting the orbital lifetime of their spacecraft and launcher stages after the end of their mission to at most 25 years in low Earth Orbit (LEO). In recent years there has been a considerable increase in space traffic due to the use of small satellites by non-traditional space operators, and due to a significant change of mission scopes and mission orbits in LEO. Many indications point to a further increase in the space traffic in LEO in the near future, including proposals for large constellations in LEO to provide broadband internet services. Several recent studies have shown that, nowadays, the guidelines for the LEO protected region are insufficiently applied by space systems of all sizes. Therefore, a substantial increase in the launch rate, whether through the large- scale release of small satellites or through the construction and maintenance of large constellations, is a potential concern for the environment and particularly if the current End of Life (EOL) behaviour prevails in the future. Even with perfect behaviour with respect to the 25 year lifetime "rule", the new traffic might lead to an extremely challenging environment trends. Furthermore, a 90% requirement for the reliability of the disposal function (ISO- 24113 standard), when weighted by the reliability of the entire system, or a failure rate of 10%, might not be sustainable if the LEO launch rates increase considerably even if these are found to be generally acceptable under current space traffic conditions. In this study, we report the results of a European effort to analyse in detail the effects that such an increase in the launch rate and number of objects in LEO would have on the space debris environment. With the use of long-term environment simulation tools, the main parameters driving the evolution of the environment under the presence of a large number of small satellites and with mega-constellations being deployed have been identified. Further analyses have been performed to identify the sensitivity of the environment to different stress parameters.

Mega-constellations, small satellites and their impact on the space debris environment

A Rossi
2016

Abstract

The number of artificial objects in orbit continues to increase and, with it, a key threat to space sustainability. In response, space agencies have identified a set of mitigation guidelines aimed at enabling space users to reduce the generation of space debris by, for example, limiting the orbital lifetime of their spacecraft and launcher stages after the end of their mission to at most 25 years in low Earth Orbit (LEO). In recent years there has been a considerable increase in space traffic due to the use of small satellites by non-traditional space operators, and due to a significant change of mission scopes and mission orbits in LEO. Many indications point to a further increase in the space traffic in LEO in the near future, including proposals for large constellations in LEO to provide broadband internet services. Several recent studies have shown that, nowadays, the guidelines for the LEO protected region are insufficiently applied by space systems of all sizes. Therefore, a substantial increase in the launch rate, whether through the large- scale release of small satellites or through the construction and maintenance of large constellations, is a potential concern for the environment and particularly if the current End of Life (EOL) behaviour prevails in the future. Even with perfect behaviour with respect to the 25 year lifetime "rule", the new traffic might lead to an extremely challenging environment trends. Furthermore, a 90% requirement for the reliability of the disposal function (ISO- 24113 standard), when weighted by the reliability of the entire system, or a failure rate of 10%, might not be sustainable if the LEO launch rates increase considerably even if these are found to be generally acceptable under current space traffic conditions. In this study, we report the results of a European effort to analyse in detail the effects that such an increase in the launch rate and number of objects in LEO would have on the space debris environment. With the use of long-term environment simulation tools, the main parameters driving the evolution of the environment under the presence of a large number of small satellites and with mega-constellations being deployed have been identified. Further analyses have been performed to identify the sensitivity of the environment to different stress parameters.
2016
Istituto di Fisica Applicata - IFAC
mega-constellations
space debris
small satellites
environment
long-term evolution
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/20.500.14243/315042
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