Directed Energy Planetary Defense

被引:1
作者
Lubin, Philip [1 ]
Hughes, Gary B. [2 ]
Bible, Johanna [1 ]
Bublitz, Jesse [1 ]
Arriola, Josh [1 ]
CaioMotta [1 ]
Suen, Jon [1 ]
Johansson, Isabella [1 ]
Riley, Jordan [1 ]
NilouSarvian [1 ]
Clayton-Warwick, Deborah [1 ]
Wu, Jane [1 ]
Milich, Andrew [1 ]
Oleson, Mitch [1 ]
Pryor, Mark [3 ,4 ]
Krogen, Peter
Kangas, Miikka [1 ]
机构
[1] Univ Calif Santa Barbara, Dept Phys, Santa Barbara, CA 93106 USA
[2] Calif Polytech State Univ San Luis Obispo, Stastist Dept, San Luis Obispo, CA 93407 USA
[3] ATK Space, Goleta, CA 93117 USA
[4] Vorticy Inc, San Diego, CA 92121 USA
来源
NANOPHOTONICS AND MACROPHOTONICS FOR SPACE ENVIRONMENTS VII | 2013年 / 8876卷
关键词
Asteroid Impact; Directed Energy; Laser Phased Array; Planetary Defense; 99942; APOPHIS; ASTEROIDS; EARTH;
D O I
10.1117/12.2030228
中图分类号
O43 [光学];
学科分类号
070207 ; 0803 ;
摘要
Asteroids and comets that cross Earth's orbit pose a credible risk of impact, with potentially severe disturbances to Earth and society. Numerous risk mitigation strategies have been described, most involving dedicated missions to a threatening object. We propose an orbital planetary defense system capable of heating the surface of potentially hazardous objects to the vaporization point as a feasible approach to impact risk mitigation. We call the system DE-STAR for Directed Energy System for Targeting of Asteroids and exploRation. DE-STAR is a modular phased array of kilowatt class lasers powered by photovoltaic's. Modular design allows for incremental development, test, and initial deployment, lowering cost, minimizing risk, and allowing for technological co-development, leading eventually to an orbiting structure that would be developed in stages with both technological and target milestones. The main objective of DE-STAR is to use the focused directed energy to raise the surface spot temperature to similar to 3,000K, allowing direct vaporization of all known substances. In the process of heating the surface ejecting evaporated material a large reaction force would alter the asteroid's orbit. The baseline system is a DE-STAR 3 or 4 (1-10km array) depending on the degree of protection desired. A DE-STAR 4 allows for asteroid engagement starting beyond 1AU with a spot temperature sufficient to completely evaporate up to 500-m diameter asteroids in one year. Small asteroids and comets can be diverted/evaporated with a DE-STAR 2 (100m) while space debris is vaporized with a DE-STAR 1 (10m).
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页数:21
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