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Removing orbital debris with lasers
Authors:Claude R. Phipps  Kevin L. Baker  Stephen B. Libby  Duane A. Liedahl  Scot S. Olivier  Lyn D. Pleasance  Alexander Rubenchik  James E. Trebes  E. Victor George  Bogdan Marcovici  James P. Reilly  Michael T. Valley
Affiliation:1. Photonic Associates, LLC, Santa Fe, NM 87508, USA;2. Lawrence Livermore National Laboratory, Livermore, CA 94550, USA;3. Centech, Carlsbad, CA 92011, USA;4. System Engineering Associates, El Segundo, CA 90245, USA;5. Northeast Science and Technology, Williamsburg, VA 23188, USA;6. Applied Systems and Material Science Department, Sandia National Laboratories, Albuquerque, NM 87185-0549, USA
Abstract:Orbital debris in low Earth orbit (LEO) are now sufficiently dense that the use of LEO space is threatened by runaway collision cascading. A problem predicted more than thirty years ago, the threat from debris larger than about 1 cm demands serious attention. A promising proposed solution uses a high power pulsed laser system on the Earth to make plasma jets on the objects, slowing them slightly, and causing them to re-enter and burn up in the atmosphere. In this paper, we reassess this approach in light of recent advances in low-cost, light-weight modular design for large mirrors, calculations of laser-induced orbit changes and in design of repetitive, multi-kilojoules lasers, that build on inertial fusion research. These advances now suggest that laser orbital debris removal (LODR) is the most cost-effective way to mitigate the debris problem. No other solutions have been proposed that address the whole problem of large and small debris. A LODR system will have multiple uses beyond debris removal. International cooperation will be essential for building and operating such a system.
Keywords:Space debris   Laser ablation   Orbital debris removal   Adaptive optics   Segmented mirror design   Phase conjugation
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