14 September 1998 Power beaming for orbital debris removal
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Proceedings Volume 3343, High-Power Laser Ablation; (1998); doi: 10.1117/12.321604
Event: High-Power Laser Ablation, 1998, Santa Fe, NM, United States
Abstract
Orbital debris in low-Earth orbit ranging in size from 1 to 10 cm in diameter can be detected but not tracked reliably enough to be easily avoided by spacecraft. In addition, shielding protection is extremely difficult and costly to accomplish for sizes above 1 - 2 cm. Debris in this size regime traveling at mean velocities on the order of 20000 miles per hour may cause catastrophic damage. Using adaptive optics technologies, a ground-based pulsed laser of sufficient power ablating the debris particle's surface to produce small momentum changes may, in several hundred pulses, lower a target debris particle's perigee sufficiently for atmospheric capture. A single laser facility could remove all of the 1 - 10 cm debris below 1500 km in altitude in approximately three years. A technology demonstration of ground based laser removal is proposed which would pave the way for the implementation of such a debris removal system. The cost of the proposed demonstration is comparable with the estimated annual cost of spacecraft operations in the present orbital debris environment.
© (1998) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Jonathan W. Campbell, Charles R. Taylor, "Power beaming for orbital debris removal", Proc. SPIE 3343, High-Power Laser Ablation, (14 September 1998); doi: 10.1117/12.321604; https://doi.org/10.1117/12.321604
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KEYWORDS
Pulsed laser operation

Satellites

Adaptive optics

Laser applications

Laser guide stars

Stars

Laser propulsion

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