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METHOD OF CHANGE OF FLIGHT TRAJECTORY OF OBJECT IN FORM OF LARGE METEORITE, ASTEROID OR COMET NUCLEUS, WITH ITS DEVIATION ASIDE FROM EARTH ORBIT
METHOD OF CHANGE OF FLIGHT TRAJECTORY OF OBJECT IN FORM OF LARGE METEORITE, ASTEROID OR COMET NUCLEUS, WITH ITS DEVIATION ASIDE FROM EARTH ORBIT
FIELD: aircraft engineering.;SUBSTANCE: invention can be used for protection of Earth against the space objects (SO). The line of the imagined circle is shaped on SO surface and evenly on a surface of the imagined dome leaning on this circle groups of charges are installed, SO is impacted by consecutive series of explosions agreed with SO geometrical sizes and density, separated from space interceptors with a control system, flight trajectory correction engines, speed levelling engines and a targeting device, groups of nuclear or thermonuclear charges of explosives spatially distributed with a detonator, liquid and the remote device of simultaneous blasting of all charges of the group in near-surface layers of meteoric and cometary substance. In top of the imagined dome the explosion of charges of larger, or equal, or smaller power is performed, and other explosions are performed with the charges of equal power. The imagined dome is formed spherical, elliptic, parabolic and any forms.;EFFECT: invention allows to change trajectory of SO flight towards Earth without destruction.;9 cl, 4 dwg
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