Thrust vectoring of an electric solar wind sail with a realistic sail shape
نویسندگان
چکیده
منابع مشابه
Electric Solar Wind Sail Mass Budget Model
The electric solar wind sail (E-sail) is a new type of propellantless propulsion system for Solar System transportation, which uses the natural solar wind for producing spacecraft propulsion. This paper discusses a mass breakdown and a performance model for 5 an E-sail spacecraft that hosts a scientific payload of prescribed mass. In particular, the model is able to estimate the total spacecraf...
متن کاملMoving an asteroid with electric solar wind sail
The electric solar wind sail (E-Sail) is a new propulsion method for interplanetary travel which was invented in 2006 and is currently under development. The E-Sail uses charged tethers to extract momentum from the solar wind particles to obtain propulsive thrust. According to current estimates, the E-Sail is 2-3 orders of magnitude better than traditional propulsion methods (chemical rockets a...
متن کاملInvited article: Electric solar wind sail: toward test missions.
The electric solar wind sail (E-sail) is a space propulsion concept that uses the natural solar wind dynamic pressure for producing spacecraft thrust. In its baseline form, the E-sail consists of a number of long, thin, conducting, and centrifugally stretched tethers, which are kept in a high positive potential by an onboard electron gun. The concept gains its efficiency from the fact that the ...
متن کاملSimulation study of solar wind push on a charged wire: basis of solar wind electric sail propulsion
One possibility for propellantless propulsion in space is to use the momentum flux of the solar wind. A way to set up a solar wind sail is to have a set of thin long wires which are kept at high positive potential by an onboard electron gun so that the wires repel and deflect incident solar wind protons. The efficiency of this so-called electric sail depends on how large force a given solar win...
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ژورنال
عنوان ژورنال: Acta Astronautica
سال: 2017
ISSN: 0094-5765
DOI: 10.1016/j.actaastro.2016.11.027