• → European Space Agency

    • About Science & Technology

    • For Public

    • For Educators

    • ESA

    • Science & Technology

    • Rosetta

    • Missions
    • Show All Missions
    • Mission Home
    • Summary
    • Fact Sheet
    • Mission Team
    • Orbit View
    • Background Science
    • 67P/C-G
    • (2867) Steins
    • (21) Lutetia
    • Asteroids
    • Map of Lutetia
    • Orbiter
    • 3D Model
    • Instruments
    • Engineering
    • Lander
    • Instruments
    • Mission Operations
    • Mission Operations
    • Launch Vehicle
    • 2nd Rosetta Launch Campaign
    • Launch Information
    • ESOC Info
    • Science Operations
    • RSOC
    • Data Archive
    • Resources
    • News Archive
    • Multimedia Gallery
    • Publication Archive
    • Calendar of Events
    • Status Report Archive
    • Services
    • Contact Us
    • Subscribe
    • Terms and Conditions
    • Bookmark and Share

    Study of the environment around the Rosetta candidate target asteroids

    Publication date: 01 Jun 1999

    Authors: Rossi, A. & Fulchignoni, M.

    Journal: Planetary and Space Science
    Volume: 47
    Issue: 6-7
    Page: pp. 873-881
    Year: 1999

    Copyright: Elsevier Science Ltd

    The Rosetta spacecraft will fly-by a few asteroids during its course to the final cometary target. The candidate asteroids presently are 3840 Ministrobel (S-type), 2703 Siwa and 140 (C-type).With the limited data presently available on these bodies we calculated some approximate quantities which may be useful to select the fly-by trajectories of the ROSETTA probe. In particular we derived the zones in which particles could stably orbit by analyzing Hills problem of three hierarchical masses--the sun, the asteroid and the orbiting particle. Then, following the approach of Hamilton and Burns, the effects of solar radiation pressure and of the ellipticity of the orbits were also taken into account. In this way for each asteroid we could calculate not only a classical quantity like the radius of the Hill sphere, but also the critical starting orbital distance (as a function of orbital inclination) within which most orbits remain bound to the asteroid, and outside which most escape as a consequence of perturbations. Moreover we determined the orbital stability zone, defined as the union of all the numerically integrated orbits showing long-term stability, for each of the target asteroids. The particular shape of these zones would suggest to have the spacecrafts close approach out of the orbital plane of the asteroids.

    Link to Publication

    Last Update: 21 Nov 2007

    • Shortcut URL
    • http://sci.esa.int/jump.cfm?oid=25209

    Connect with us

    • RSS
    • Youtube
    • Twitter
    • Flickr
    • Google Buzz
    • Livestream
    • Subscribe
    • App Store
    • ESA Science Twitter

    Follow ESA science

    • Copyright 2000 - 2013 © European Space Agency. All rights reserved.

    • Terms and Conditions