End-of-life disposal of spacecraft in highly elliptical orbits by means of luni-solar perturbations and Moon resonances (Contributo in atti di convegno)

Type
Label
  • End-of-life disposal of spacecraft in highly elliptical orbits by means of luni-solar perturbations and Moon resonances (Contributo in atti di convegno) (literal)
Anno
  • 2013-01-01T00:00:00+01:00 (literal)
Alternative label
  • C. Colombo, E.M. Alessi, M. Landgraf (2013)
    End-of-life disposal of spacecraft in highly elliptical orbits by means of luni-solar perturbations and Moon resonances
    in 6th European Conference on Space Debris, Darmstadt, Germany, 22-25 April 2013
    (literal)
Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#autori
  • C. Colombo, E.M. Alessi, M. Landgraf (literal)
Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#affiliazioni
  • University of Southampton (U.K.), IFAC-CNR (Italy), ESA/ESOC (Germany) (literal)
Titolo
  • End-of-life disposal of spacecraft in highly elliptical orbits by means of luni-solar perturbations and Moon resonances (literal)
Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#isbn
  • 978-92-9221-287-2 (literal)
Abstract
  • This paper presents a preliminary investigation of some possible strategies for the disposal of spacecraft on Highly Elliptical Orbits at the end-of-life. The effect of luni-solar perturbations is analysed through a simplified phase space model. This allows identifying the conditions for re-entry in the Earth's atmosphere. As a second strategy, Moon resonances are studied to increase the orbit perigee and transfer the spacecraft on weak capture orbits. (literal)
Prodotto di
Autore CNR

Incoming links:


Prodotto
Autore CNR di
data.CNR.it