On an idea about the method of absorbing spin motion of an asteroid for capture

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Narita, Shin Ichiro
Teramoto, Yuki
Kikuchi, Shota
Mizumori, Tsukasa
Kawaguchi, Jun Ichiro

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Univelt Inc.

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This paper presents a method to remove the spin of a target asteroid for a capture mission. The idea uses a small robotic spacecraft either launched separately or carried on the larger mother spacecraft. The small spacecraft first winds up a tether around the target asteroid while itself playing the role of a tip mass, as in a Yo-Yo mechanism. The operation may rely on sophisticated robotic technology, and may include the surface mobile agent jettisoned from the spacecraft.

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Astrodynamics 2013 - Advances in the Astronautical Sciences: Proceedings of the AAS/AIAA Astrodynamics Specialist Conference

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