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Design of a novel nozzle for rocket engines with full flow at sea level

Crossref DOI link: https://doi.org/10.1007/s00193-025-01236-2

Published Online: 2025-06-29

Published Print: 2025-08

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

Authors

Liu, Y. Z. https://orcid.org/0000-0002-6409-4427
Wang, Z. https://orcid.org/0000-0001-9235-7725
Li, P. https://orcid.org/0000-0003-0469-7549
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Text and Data Mining valid from 2025-06-29

Version of Record valid from 2025-06-29
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Article History

Received: 16 July 2022

Revised: 21 December 2023

Accepted: 23 May 2025

First Online: 29 June 2025