Computational Investigation of Fluidic Thrust Vectoring Control in Modified Vikas Nozzle

Over the decades, polar satellite launch vehicles and geosynchronous launch vehicles have utilized variants of the Vikas engine for numerous space operations. The pitching control for those launch vehicles is achieved by gimbaling the Vikas engine nozzle up to ± 4° with mechanical actuating parts. T...

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Bibliographic Details
Main Authors: T. Harish Ragavendra, P. A. Anupama, K. S. Jai Pranesh, D. Lakshmanan, R. Abinaya
Format: Article
Language:English
Published: Isfahan University of Technology 2025-01-01
Series:Journal of Applied Fluid Mechanics
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Online Access:https://www.jafmonline.net/article_2583_71db1eecd3a4d7db88a3e56a223d6b1f.pdf
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