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Elsevier, Acta Astronautica

DOI: 10.1016/j.actaastro.2017.11.028

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Utilization of thermite energy for re-entry disruption of detachable rocket elements made of composite polymeric material

This paper was not found in any repository, but could be made available legally by the author.
This paper was not found in any repository, but could be made available legally by the author.

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