Abstract
During the last 40 years, the mass of orbiting objects increased at the rate of about 145 metric tons annually, leading to a total of approximately 7000 metric tons. Most of the cross-sectional area and mass (97% in low Earth orbit, LEO) is concentrated in about 4500 intact objects, i.e. abandoned spacecraft and rocket bodies, plus a further 1000 operational spacecrafts. Numerical simulations show that the most effective way to prevent an exponential growth of the cataloged debris population would be to remove enough cross-sectional area and mass from densely populated orbits. According to the most recent NASA results, the active yearly removal of approximately 0.1% of the abandoned intact objects would be sufficient to stabilize the cataloged debris in LEO. The typical targets for removal would have masses between 500 and 1000 kg, for spacecraft, and of more than 1000 kg, for rocket upper stages. This paper investigates a space mission concept for active removal of abandoned Cosmos-3M second stages from LEO. The proposed concept relies on flying a multi-removal space platform carrying a number of Hybrid Propulsion Modules (HPMs). After capture, a HPM is installed on the debris, which is then de-orbited in a controlled fashion. The estimated mass of a single HPM results about 200 kg, making possible a multi-removal mission by means of a low-cost class-launcher.
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References
IADC Steering Group, “Space debris: IADC assessment report for 2010”, Inter-Agency Space Debris Coordination Committee (IADC), 2012.
J.-C. Liou, “An active debris removal parametric study for LEO environment remediation”, Advances in Space Research, Vol. 47, pp. 1865–1876, 2011.
UNCOPUOS. “Space debris mitigation guidelines of the United Nations Committee on the Peaceful Uses of Outer Space”, A/62/20 (2007), Endorsed by the General Assembly Resolution A/RES/62/217, United Nations, New York, USA, 2008.
IADC Steering Group & Working Group 4, “Space debris mitigation guidelines”. IADC-02-01, rev. 1, Inter-Agency Space Debris Coordination Committee (IADC), 2007.
C. Pardini, L. Anselmo, “Assessment of the consequences of the Fengyun-1C breakup in low Earth orbit”, Advances in Space Research, Vol. 44, pp. 545–557, 2009.
C. Pardini, L. Anselmo, “Physical properties and long-term evolution of the debris clouds produced by two catastrophic collisions in Earth orbit”, Advances in Space Research, Vol. 48, pp. 557–569, 2011.
A. Rossi, L. Anselmo, C. Pardini, G.B. Valsecchi, R. Jehn, “The new Space Debris Mitigation (SDM 4.0) long-term evolution code, Proceedings of the 5th European Conference on Space Debris, ESA SP-672, CDROM, European Space Agency, Noordwijk, The Netherland, 2009.
J.-C. Liou, N-L. Johnson, “A sensitivity study of the effectiveness of active debris removal in LEO”, Acta Astronau-tica, Vol. 64, pp. 236–243, 2009.
J.-C. Liou, N-L. Johnson, “Controlling the growth of future LEO debris populations with active debris removal”, Acta Astronautica, Vol. 66, pp. 236–243, 2010.
H. Burkhardt et al, “Evaluation of propulsion systems for satellite end of life de-orbiting”, AIAA Paper, AIAA-2002-4208, 2002.
L.T. DeLuca et al, “Active space debris removal by hybrid propulsion module”, Acta Astronautica, Vol. 91, pp. 20–33, 2013.
D. Accardo, G. Fasano, and M. Grassi, “Vision-based Relative Navigation”, Distributed Space Missions for Earth System, Monitoring. Space Technology Library, Vol. 31, pp. 267–305, 2013.
F. Branz et al, “Soft docking system for capture of irregularly shaped, uncontrolled space objects”, 6th European Conference on Space Debris, ESA/ESOC, Darmstadt, Germany, 2013.
P. Tadini, F. Maggi, L.T. DeLuca, C. Pardini, L. Anselmo, M. Grassi, V. Trushlyakov. “Active Debris Removal of a Cosmos-3M second stage by Hybrid Rocket Module”, VIII International Science and Technology Conference “Dynamics of Systems, Mechanisms and Machines”, Omsk, Russian Federation, 2012.
R. Janovsky, M. Kassebom, H. Lubbersted and O. Romberg. “End-Of-Life De-Orbiting Strategies for Satellites”, Deutscher Luft- und Raumfahrtkongress, DGLR-JT2002-028, 2002.
D. Altman, “Highlights in Hybrid Rocket Propulsion History”, The 10th International Workshop on Combustion and Propulsion, Lerici-La Spezia, Italy, 2003.
S. Gordon, B.J. McBride, “Computer Program for Calculation of Complex Chemical Equilibrium Composition and Applications I. Analysis”, NASA Reference Publications 1311, 1994.
M.J. Chiaverini, K.K. Kuo, “Fundamentals of Hybrid Rocket Combustion and Propulsion”, AIAA Progress in Astronautics and Aeronautics, Vol. 218, pp. 37–125, 2007.
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DeLuca, L.T., Lavagna, M., Maggi, F. et al. Large Debris Removal Mission in LEO based on Hybrid Propulsion. Aerotec. Missili Spaz. 93, 51–58 (2014). https://doi.org/10.1007/BF03404676
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DOI: https://doi.org/10.1007/BF03404676