he feasibility of a mission for the active removal of a large massive debris in Low Earth Orbit region is investigated. Critical aspects and related technologies are investigated at preliminary level. A preliminary mass budget shows that the chaser spacecraft overall mass varies in the range 1500-1700 kg, with Hybrid Propulsion Module of about 900 kg

Large-debris active removal challenge: the hybrid propulsion approach

FRANCESCONI, ALESSANDRO;
2013

Abstract

he feasibility of a mission for the active removal of a large massive debris in Low Earth Orbit region is investigated. Critical aspects and related technologies are investigated at preliminary level. A preliminary mass budget shows that the chaser spacecraft overall mass varies in the range 1500-1700 kg, with Hybrid Propulsion Module of about 900 kg
2013
Proceedings 57th Symposium on Space Science and Technology
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11577/2891099
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