We present the main findings of a dynamical mapping performed in the Low Earth Orbit region. The results were obtained by propagating an extended grid of initial conditions, considering two different epochs and area-to-mass ratios, by means of a singly averaged numerical propagator. It turns out that dynamical resonances associated with high-degree geopotential harmonics, lunisolar perturbations and Solar radiation pressure can open natural deorbiting highways. For area-to-mass ratios typical of the orbiting intact objects, these corridors can be exploited only in combination with the action exerted by the atmospheric drag. For satellites equipped with an area augmentation device, we show the boundary of application of the drag, and where the Solar radiation pressure can be exploited.

Natural highways for end-of-life solutions in the LEO region

Alessi Elisa Maria;Schettino Giulia;Rossi Alessandro;Valsecchi Giovanni B
2018

Abstract

We present the main findings of a dynamical mapping performed in the Low Earth Orbit region. The results were obtained by propagating an extended grid of initial conditions, considering two different epochs and area-to-mass ratios, by means of a singly averaged numerical propagator. It turns out that dynamical resonances associated with high-degree geopotential harmonics, lunisolar perturbations and Solar radiation pressure can open natural deorbiting highways. For area-to-mass ratios typical of the orbiting intact objects, these corridors can be exploited only in combination with the action exerted by the atmospheric drag. For satellites equipped with an area augmentation device, we show the boundary of application of the drag, and where the Solar radiation pressure can be exploited.
2018
Istituto di Fisica Applicata - IFAC
Inglese
130
5
22
Sì, ma tipo non specificato
Eccentricity growth
Resonances
LEO
Passive mitigation
SRP
Space debris
4
info:eu-repo/semantics/article
262
Alessi, ELISA MARIA; Schettino, Giulia; Rossi, Alessandro; Valsecchi Giovanni, B
01 Contributo su Rivista::01.01 Articolo in rivista
none
   Revolutionary Design of Spacecraft through Holistic Integration of Future Technologies
   ReDSHIFT
   H2020
   687500
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/20.500.14243/374512
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