Authors: Alexander Bolonkin
For Protection of the Earth from asteroid we need in methods for changing the asteroid trajectory and theory for an estimation or computation the impulse which produces these methods. Author develops some methods of this computation. There are: impact of the space apparatus to asteroid, explosion the conventional explosive having form of plate and ball on asteroid surface, explosion the small nuclear bomb on the asteroids surface, entry asteroid to Earth atmosphere, braking of asteroid by parachute. Offered method may be also used for braking of apparatus reentering in the Earth from a space flight. The offered theory also may be used for protection the Earth from impact of a big asteroid.
Comments: 7 Pages.
[v1] 2012-12-01 20:06:13
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