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What is Drag Coefficient of Suborbital Rocket Model about?

This study presents the design of a test section for measuring the drag coefficient of suborbital rocket models at a Mach number of 2.45, utilizing numerical simulations and wind tunnel tests. The research highlights discrepancies between simulated and measured drag forces, prompting further analysis of the test section and force measurement system. The findings aim to optimize drag evaluation and improve the design of suborbital rockets, specifically the PERUN rocket being developed by SpaceForest.

Author

39SEAShashi Khatri

Language

EN