Project “space sheppard” with ion beam. ideas and problems
|1Bombardelli, C, 2Alpatov, AP, 3Pirozhenko, AV, 4Baranov, EYu., 4Osinovyj, GG, 5Zakrzhevskii, AE |
1Madrid Technical University, Madrid, Spain
2Institute of Technical Mechanics of the National Academy of Science of Ukraine and the State Space Agency of Ukraine, Dnipropetrovsk, Ukraine
3Institute of Technical Mechanics of the NAS of Ukraine and SSA of Ukraine, Dnipro, Ukraine
4Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine
5S.P. Timoshenko Institute of Mechanics of the National Academy of Sciences of Ukraine, Kyiv, Ukraine
|Kosm. nauka tehnol. 2014, 20 ;(2):55–60|
|Section: Space Environment Monitoring and Space Debris|
|Publication Language: Russian|
We give some short information on objectives and problems of the international project LEOSWEEP that is performed by a set of Ukrainian organizations in collaboration with leading European space organizations. The project deals with development of the first space mission directed on the contactless deorbiting of upper stages of launchers.
|Keywords: deorbiting of launchers, project LEOSWEEP|
1. Alpatov A. P., Bass V. P., Baulin S. A. et al. Debris in near-Earth space. Ed. A. P. Alpatova, 378 p. (Porogi, Dnepropetrovsk, 2012) [in Russian].
2. Bombardelli C., Herrera J., Iturri A., Peláez J.Space debris removal with bare electrodynamic tethers. Proceedings of the 20th AAS/AIAA Spaceflight Mechanics Meeting. (San Diego, CA, 2010).
3. Bombardelli C., Peláez J.Ion beam Shepherd for contactless space debris removal. J. Guidance, Contr., and Dynamics. 34(3), 916—920 (2011).
4. Bondarenko S., Lyagushin S., Shifrin G.Prospects of using lasers and military space technology for space debris removal. Second European Conference on Space Debris. 393, P. 703 (1997).
5. Levin E. M. Dynamic analysis of space tether missions. Adv. Astronaut. Sci. 453 p. (2007).
6. Phipps C. R., Reilly J. P.ORION: Clearing near-Earth space debris in two years Using a 30-kW repetitively-pulsed laser. SPIE Proceedings of the International Society for Optical Engineering. P. 728—731 (1997).
7. Sanjurjo-Rivo M.Self-balanced bare electrodynamic tethers. Space debris mitigation and other applications: Ph. D. Thesis. (Technical Univ. of Madrid, School of Aeronautics, 2009).
8. Takeichi N.Practical operation strategy for deorbit of an electrodynamic tethered system. J. Spacecraft and Rockets. 43(6), P. 1283—1288 (2006). doi:10.2514/ 1.19635.
9. Technicalreport on space debris, United Nations. 50 p. (New York, 1999).
10. Todd L., Bowling T.Debris mitigation in geostationary Earth orbit. Sixth Dynamics and Control of Systems and Structures in Space Conference, Riomaggiore, Italy, July (2004).