Optimal options for rendezvous and impact missions to NEOs

Massimiliano Vasile, Paolo De Pascale, Stefano Casotto

Research output: Contribution to journalArticle

3 Citations (Scopus)

Abstract

In this paper some potentially interesting transfer options for missions to Near Earth Objects have been studied. Due to thehigh number of potential targets and to the large variety of possible missions that can be considered, especially if resorting to low-thrust propulsion, an extensive analysis of transfer options requires a preliminary approach oriented toward an effective global search, and an appropriately simplified trajectory transcription. Low-thrust options have been modeled through a novel shape-based approach and a global optimization method has been used to look for globally optimal transfers. Different targets have been identified and various mission scenarios have been considered: rendezvous, sample return missions both with and without Earth gravity assist and impact missions.
LanguageEnglish
Number of pages9
JournalJBIS, Journal of the British Interplanetary Society
Volume59
Issue number11
Publication statusPublished - Nov 2006

Fingerprint

near Earth objects
rendezvous
thrust
Earth (planet)
Global optimization
Transcription
Propulsion
Gravitation
low thrust propulsion
trajectory
Trajectories
sample return missions
gravity
low thrust
trajectories
gravitation
optimization
method
analysis

Keywords

  • neo
  • impact missions
  • sample and return
  • space missions
  • near earth objects

Cite this

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Optimal options for rendezvous and impact missions to NEOs. / Vasile, Massimiliano; De Pascale, Paolo; Casotto, Stefano.

In: JBIS, Journal of the British Interplanetary Society, Vol. 59, No. 11, 11.2006.

Research output: Contribution to journalArticle

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