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Methodology for Estimation of Shock Wave and Acoustic Loading of a Designed Rocket Block Equipped with an Aerospike Engine at the Landing Stage

Published Online: 2025-01-14

Published Print: 2024-09

Authors

Peshkov, R. A.

Tret’yakov, P. A.
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Text and Data Mining valid from 2024-09-01

Version of Record valid from 2024-09-01
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Article History

Received: 6 June 2024

Revised: 7 July 2024

Accepted: 9 July 2024

First Online: 14 January 2025

CONFLICT OF INTEREST

: The authors of this work declare that they have no conflicts of interest.

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