Trajectory Design with Hybrid Low-Thrust Propulsion System
نویسندگان
چکیده
منابع مشابه
Trajectory Design with Hybrid Low-Thrust Propulsion System
Anovelmission concept based on ahybrid low-thrust propulsion system is proposed anddiscussed.A solar electric propulsion thruster is coupled with an auxiliary system providing an inverse square radial thrust. In this way the spacecraft is virtually subjected to a reduced gravitational solar force. The primary purpose of this paper is to quantify the impact of the reduced solar force on the prop...
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ژورنال
عنوان ژورنال: Journal of Guidance, Control, and Dynamics
سال: 2007
ISSN: 0731-5090,1533-3884
DOI: 10.2514/1.22433