Asteroid Deflection: How, where and when?
D. Fargion

TL;DR
This paper proposes a novel asteroid deflection method using multi screw-rockets with mini-nuclear engines to eject soil and increase momentum exchange, potentially deflecting dangerous asteroids like Apophis safely.
Contribution
It introduces a new asteroid deflection technique involving lander-based soil ejection with mini-nuclear engines, enhancing momentum transfer and enabling safe deflection.
Findings
Proposes a feasible method for asteroid deflection using soil ejection.
Suggests the approach can safely deflect asteroids like Apophis.
Highlights potential for asteroid-based space infrastructure development.
Abstract
To deflect impact-trajectory of massive km^3 and spinning asteroid by a few terrestrial radius one need a large momentum exchange. The dragging of huge spinning bodies in space by external engine seems difficult or impossible. Our solution is based on the landing of multi screw-rockets, powered by mini-nuclear engines, on the body, that dig a small fraction of the soil surface, to use as an exhaust propeller, ejecting it vertically in phase among themselves. Such a mass ejection increases the momentum exchange, their number redundancy guarantees the stability of the system. The slow landing (below 40 cm s^-1) of each engine-unity at those lowest gravity field, may be achieved by save rolling and bouncing along the surface. The engine array tuned activity, overcomes the asteroid angular velocity. Coherent turning of the jet heads increases the deflection efficiency. A procession along…
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Taxonomy
TopicsAstro and Planetary Science · Planetary Science and Exploration
