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 / P., T.P., F., M., M., L., L. T., D.L., Grassi, M., C., P., L., A., A., F., N., V., U., T.. - (2013), pp. 1-6. (57th Symposium on Space Science and Technology Yonago, Japan 9-11 October 2013).

Large-debris active removal challenge: the hybrid propulsion approach

GRASSI, MICHELE;
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.
2013
Large-debris active removal challenge: the hybrid propulsion approach / P., T.P., F., M., M., L., L. T., D.L., Grassi, M., C., P., L., A., A., F., N., V., U., T.. - (2013), pp. 1-6. (57th Symposium on Space Science and Technology Yonago, Japan 9-11 October 2013).
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11588/577517
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