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Experimental and theoretical investigation of combustion efficiency, regression rate, and thrust characteristics of a hybrid rocket engine using PVC/DBP fuel

Crossref DOI link: https://doi.org/10.1007/s42401-025-00392-8

Published Online: 2025-08-04

Published Print: 2026-03

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

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