SPACE DEBRIS MITIGATION MEASURES APPLIED TO EUROPEAN LAUNCHERS
- Paper number
IAC-08.A6.4.4
- Author
Mr. Christophe Bonnal, Centre National d'Etudes Spatiales (CNES), France
- Coauthor
Mr. Didier AUBIN, Arianespace, France
- Coauthor
Mr. Jacques Gigou, European Space Agency (ESA), France
- Year
2008
- Abstract
In November 1986, more than 20 years ago, an H8 upper stage of Ariane 1 exploded in orbit nine months after the end of its mission. So as to avoid the generation of debris in low earth orbit, a dedicated complementary development modified the design, introducing systematic passivation of the stage. Ever since this event, space debris mitigation has been a major concern for all launcher activities in Europe. After a short recall of the launchers currently operated by Arianespace as well as those currently developed by ESA with CNES, particularly for the safeguard authority, including the most promising future evolutions, the set of applicable regulations is described. These rules are fundamentally derived from the IADC Guidelines (hence the UNCOPUOS ones), translated into European Code of Conduct and in some more applicable Standards, such as the one prepared by ESA. The process of preparing ISO standards, mainly through the ECSS Working Group, is also described. Three major families can be identified: minimization of Mission Related Objects, Passivation of stages at the end of mission, and orbital protected zones including the so-called 25 years rule. The paper describes how European launchers do or will fulfill these applicable standards, quantifying the efficiency of the mitigation rules, and describing improvement actions currently under study.
- Abstract document
- Manuscript document
IAC-08.A6.4.4.pdf (🔒 authorized access only).
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