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Sensitivity Analysis of the Key Design Parameters of Turbomachinery in the Closed Helium Cycle System of Pre-cooling Air Turbo Rocket Engine.

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Bibliographic Details
Title: Sensitivity Analysis of the Key Design Parameters of Turbomachinery in the Closed Helium Cycle System of Pre-cooling Air Turbo Rocket Engine.
Authors: Zhao, Zeyang1,2 (AUTHOR), Zhao, Xiaotian1 (AUTHOR), Ma, Haibo3 (AUTHOR), Nan, Xiangyi3 (AUTHOR), Liu, Jinxin1 (AUTHOR)
Source: EPJ Web of Conferences. 4/13/2026, Vol. 361, p1-11. 11p.
Database: Academic Search Ultimate
Description
ISSN:21016275
DOI:10.1051/epjconf/202636105001