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Improving the completeness of combustion of boron particles in a solid-fuel ducted rocket owing to distributed air supply to the secondary combustor

Crossref DOI link: https://doi.org/10.1134/S0012501616120034

Published Online: 2017-01-06

Published Print: 2016-12

Update policy: https://doi.org/10.1007/springer_crossmark_policy

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