Discussion on Momentum Transfer Difficulty of a Magnetoplasma Sail
Author:
Affiliation:
1. Tokyo University of Agriculture and Technology, Tokyo 184-8588, Japan
2. Japan Aerospace Exploration Agency, Kanagawa 252-5210, Japan
3. Nagoya University, Nagoya 464-8601, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B34141
Reference9 articles.
1. Mini-Magnetospheric Plasma Propulsion: Tapping the energy of the solar wind for spacecraft propulsion
2. Magneto-plasma sail: An engineering satellite concept and its application for outer planet missions
3. Fundamentals of the Plasma Sail Concept: Magnetohydrodynamic and Kinetic Studies
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2. Control of the drag on a spacecraft in the earth’s ionosphere using the spacecraft’s magnetic field;Acta Astronautica;2018-10
3. Braking of a “Magnetized” Sphere in a Hypersonic Rarefied Plasma Flow;High Temperature;2018-07
4. Experimental Investigation of Magnetoplasma Sail with High Beta Plasma Jet;50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference;2014-07-25
5. The Use of Dipole Plasma Equilibrium for Magnetic Sail Spacecraft;Fusion Science and Technology;2013-05
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