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A laser-optical system to re-enter or lower low Earth orbit space debris
Institution:1. Hosei University, Tokyo, Japan;2. Japan Aerospace Exploration Agency, Tokyo, Japan;1. GMV, Spain;2. GMV, Romania;3. Politecnico di Milano, Italy;4. Fundación PRODINTEC, Spain;5. European Space Agency (ESA), The Netherlands;1. IZEST, École Polytechnique, 91128 Palaiseau, France;2. IZEST, CEA-Saclay, DSM-IRAMIS-SPAM bât. 522 p. 148, 91191 Gif-sur-Yvette, France;3. Dept. of Physics and Astronomy, University of California at Irvine, Irvine, CA 92697, USA
Abstract:Collisions among existing Low Earth Orbit (LEO) debris are now a main source of new debris, threatening future use of LEO space. Due to their greater number, small (1–10 cm) debris are the main threat, while large (>10 cm) objects are the main source of new debris. Flying up and interacting with each large object is inefficient due to the energy cost of orbit plane changes, and quite expensive per object removed. Strategically, it is imperative to remove both small and large debris. Laser-Orbital-Debris-Removal (LODR), is the only solution that can address both large and small debris. In this paper, we briefly review ground-based LODR, and discuss how a polar location can dramatically increase its effectiveness for the important class of sun-synchronous orbit (SSO) objects. With 20% clear weather, a laser-optical system at either pole could lower the 8-ton ENVISAT by 40 km in about 8 weeks, reducing the hazard it represents by a factor of four. We also discuss the advantages and disadvantages of a space-based LODR system. We estimate cost per object removed for these systems. International cooperation is essential for designing, building and operating any such system.
Keywords:Space debris  Laser ablation  Laser-produced plasma
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