METHOD OF ASTEROID ORBIT DEFLECTION (VERSIONS) Russian patent published in 2014 - IPC B64G99/00 

Abstract RU 2533778 C2

FIELD: aircraft engineering.

SUBSTANCE: several nuclear or neutron charges are forced towards front or lateral sides of stone, reinforced concrete or metallic asteroid, charge power not breaking the asteroid integrity. The last charge to be launched is nuclear charge or neutron charge or thermonuclear charge in power sufficient to break the asteroid integrity.

EFFECT: ruled out collision with the Earth.

4 cl

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RU 2 533 778 C2

Authors

Staroverov Nikolaj Evgen'Evich

Dates

2014-11-20Published

2013-03-04Filed