THE ROCKET CONCEPTION OF CUMULATIVE IMPACT DEFENSE OF THE EARTH AGAINST DANGEROUS SPACE OBJECTS

Citation
As. Alekseev et al., THE ROCKET CONCEPTION OF CUMULATIVE IMPACT DEFENSE OF THE EARTH AGAINST DANGEROUS SPACE OBJECTS, International journal of impact engineering, 20(1-5), 1997, pp. 1-12
Citations number
2
ISSN journal
0734743X
Volume
20
Issue
1-5
Year of publication
1997
Pages
1 - 12
Database
ISI
SICI code
0734-743X(1997)20:1-5<1:TRCOCI>2.0.ZU;2-4
Abstract
Asteroids and comets with trajectories intersecting of the Earth repre sent a danger to our planet. Possible ways to prevent a dangerous obje ct from colliding with Earth are splitting or deflecting its trajector y. For that purpose nuclear explosive devices with power up to 10-20 M egatons are proposed to be used. The report based on statistical data processing embracing over 100 potentially dangerous asteroids gives a substantiation of required performances of the Space Rocket Intercepti on Complex - the basic component of the Earth Protection System. The c alculated time of interception and required initial velocity, dependin g on the time left until collision and efficiency of the available nuc lear device, are presented. The report shows the possibility of creati ng an interception complex consisting of a space interceptor with a nu clear explosive device, a booster, a launch-vehicle and supporting sys tems.