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Optimum Design of Liquid Fuel Launch Vehicle Based on Design of Missile Under Uncertainty with Latin Hyper-cube Method (LHS)

Published Online: 2024-12-31

Published Print: 2025-07

Authors

Shalmaee, Maziar Hoseini

Toloei, Alireza

Nosratollahi, Mehran
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Text and Data Mining valid from 2024-12-31

Version of Record valid from 2024-12-31
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Article History

Received: 10 June 2024

Revised: 1 December 2024

Accepted: 11 December 2024

First Online: 31 December 2024

Declarations

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: On behalf of all authors, the corresponding author states that there is no conflict of interest.

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