The 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
Pardini C;Anselmo L;
2013
Abstract
The 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.File in questo prodotto:
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Descrizione: Large-Debris Active Removal Challenge: the Hybrid Propulsion Approach
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