Continuous thrust tangential or perpendicular to the flight direction on a given transfer trajectory in planar Circular Restricted 3-Body Problem

This paper presents a systematic study for analytical determination of thrust acceleration magnitude on a given trajectory for a case where the thrust is tangential or perpendicular to the flight direction. The problem has been formulated using the planar Circular Restricted Three-Body Problem. In t...

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Bibliographic Details
Main Author: Mircea DUMITRACHE
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2011-06-01
Series:INCAS Bulletin
Subjects:
Online Access:http://bulletin.incas.ro/files/dumitrache_mircea_v3_is2_full.pdf