http://www.cnr.it/ontology/cnr/individuo/prodotto/ID91389
Influence of high eccentricity objects on the evolution of the geo environment (Contributo in atti di convegno)
- Type
- Label
- Influence of high eccentricity objects on the evolution of the geo environment (Contributo in atti di convegno) (literal)
- Anno
- 2009-01-01T00:00:00+01:00 (literal)
- Alternative label
Rossi A.; Anselmo L.; Pardini C. (2009)
Influence of high eccentricity objects on the evolution of the geo environment
in Fifth European Conference on Space Debris, Darmstadt, Germania, 30/3 - 2/4, 2009
(literal)
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- Rossi A.; Anselmo L.; Pardini C. (literal)
- Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#titoloVolume
- Fifth European Conference on Space Debris (literal)
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- Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#note
- In: Fifth European Conference on Space Debris (Darmstadt, Germania, 30 March - 2 April 2009). Proceedings, vol. ESA SP-672 (CD-ROM) article n. 3. H. Lacoste (ed.). ESA Communication Production Office, ESTEC, 2009. (literal)
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- ABSTRACT: The long term influence of objects crossing or abandoned in GEO was evaluated, based on current practices, using the new Space Debris Mitigation model SDM 4.0. It was the latest version of a long term evolution code originally developed in the early 1990's, specifically designed to model with high accuracy the high Earth orbit regimes. Starting from the MASTER-2005 debris population, the long term evolution of the GEO environment was simulated under a few realistic scenarios, based on increasingly aggressive mitigation strategies. Beyond the high eccentricity objects, also the influence of the rocket stages separated from GEO spacecraft and left in geosynchronous drift orbits was analyzed. The main mitigation measures considered included the re-orbiting of GEO spacecraft at the end-of-life in the super-GEO graveyard zone, the de-orbiting of GTO/HEO upper stages and the re-orbiting of the rocket stages usually abandoned in drift orbits. These simulations allowed the quantitati (literal)
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- Titolo
- Influence of high eccentricity objects on the evolution of the geo environment (literal)
- Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#isbn
- 978-0-521-85203-6 (literal)
- Abstract
- The long term influence of objects crossing or
abandoned in GEO was evaluated, based on current
practices, using the new Space Debris Mitigation model
SDM 4.0. It was the latest version of a long term
evolution code originally developed in the early 1990's,
specifically designed to model with high accuracy the
high Earth orbit regimes.
Starting from the MASTER-2005 debris population, the
long term evolution of the GEO environment was
simulated under a few realistic scenarios, based on
increasingly aggressive mitigation strategies. Beyond
the high eccentricity objects, also the influence of the
rocket stages separated from GEO spacecraft and left in
geosynchronous drift orbits was analyzed. The main
mitigation measures considered included the re-orbiting
of GEO spacecraft at the end-of-life in the super-GEO
graveyard zone, the de-orbiting of GTO/HEO upper
stages and the re-orbiting of the rocket stages usually
abandoned in drift orbits.
These simulations allowed the quantitative estimation of
the collision probability related to all the above
mentioned classes of objects. The effectiveness of the
current mitigation measures was assessed and the
rationale of new mitigation guidelines devised to
minimize the future collision risk in GEO was
discussed. (literal)
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