Removing orbital debris with lasers |
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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 |
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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 |
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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. |
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Keywords: | Space debris Laser ablation Orbital debris removal Adaptive optics Segmented mirror design Phase conjugation |
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