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Anatoliy Kostyuk: METHOD FOR PROTECTING THE EARTH AGAINST ASTEROID-COMET HAZARD

Anatoliy Kostyuk: METHOD FOR PROTECTING THE EARTH AGAINST ASTEROID-COMET HAZARD

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Basic Information
Anatoliy Kostyuk: METHOD FOR PROTECTING THE EARTH AGAINST ASTEROID-COMET HAZARD
  • Foundation date

    30 July 2009

Abstract

 1. A method of protecting the Earth from an asteroid-comet hazard, namely, that a spacecraft is directed towards a dangerous celestial body, equipped with means to influence a dangerous celestial body to change its flight path, characterized in that the spacecraft is equipped with a device for receiving a moving external inertial forces directed in a given direction, acting without force interaction with the environment and without mass loss, report the motion to the spacecraft using a driving external inertia force and a device for generating a driving external inertia force is supplied from a nuclear energy source or from a solar battery-based power source, sets the spacecraft to move along a path that involves the spacecraft flying away from the Earth a given distance, turning the spacecraft and moving it toward the Earth in such a way that the trajectory and speed of the spacecraft are close after a given time to the trajectory and speed of a dangerous celestial body, the cosmos will approach Cesky vehicle with dangerous celestial body and have the dangerous heavenly body lateral force effect until a new trajectory of its flight, in which the dangerous celestial body fly past Earth at a safe distance. ! 2. The method according to claim 1, characterized in that the spacecraft-interceptor is launched from the spacecraft to approach the dangerous celestial body and force impact on it, control this device from the spacecraft until a new flight path of the dangerous celestial body is received. ! 3. The method according to claim 2, about

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Priorities

Application RU2009129382/11A events 

2009-07-30

Application filed by Анатолий Иванович Костюк (RU), Анатолий Иванович КОСТЮК

2009-07-30

Priority to RU2009129382/11A

2011-02-10

Publication of RU2009129382A