Abstract
This paper describes the activities performed by Aviospace in the frame of CADET (CApture and DE-orbiting Technologies) R&T project, whose objective is the preliminary development of enabling technologies required for Active Debris Removal from LEO orbits. The project focuses in particular in-space capture concepts for large space debris, such as upper stages of elderly launchers or decommissioned satellites. For these, a non-collaborative rendez-vous and capture procedure, to be performed by a robotic spacecraft (namely “chaser”), is required.
Such enabling technologies include:
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techniques for orbital recognition of the target debris, based on images obtained in-situ by the chaser spacecraft via optical sensors
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technologies of autonomous guidance, navigation and control for phases of close rendez-vous, final approach and capture
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technologies, strategies and concepts for target capture and solidarization
For such technologies, current level of development – at least on the national scenario - is TRL 2 and it is planned to reach of TRL 4 through the development of an integrated demonstrator and the associated test setup to be adopted for functional validation.
CADET project started in January 2013; it is co-funded by Regione Piemonte according to: POR FESR 2007/2013 – linea di attività I.1.1. “Piattaforme innovative” – AEROSPAZIO FASE II.
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References
NASA, “Handbook for Limiting Orbital Debris”, Washington DC, 2008
J.C. Liou, D.T. Hall, P.H. Krisko, J.N. Opiela, “LEGEND, a 3-dimensional LEO to GEO Debris Evolutionary Model”, Adv. Space Res., 2004
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© 2015 Springer International Publishing Switzerland
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Chiesa, A., Fossati, F., Gambacciani, G., Pensavalle, E. (2015). Enabling Technologies for Active Space Debris Removal: The Cadet Project. In: Sgobba, T., Rongier, I. (eds) Space Safety is No Accident. Springer, Cham. https://doi.org/10.1007/978-3-319-15982-9_4
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DOI: https://doi.org/10.1007/978-3-319-15982-9_4
Publisher Name: Springer, Cham
Print ISBN: 978-3-319-15981-2
Online ISBN: 978-3-319-15982-9
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