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What is Satellite Carrier Aerodynamics Study about?

This study analyzes the structure and aerodynamic properties of a low altitude satellite carrier system to determine optimal parameters for its delivery. Using Computational Fluid Dynamics (CFD), the research calculates drag forces and coefficients across a range of Mach numbers, revealing a drag coefficient of 0.342 at M = 0.6 and 7.65 at M = 4. The findings indicate that the actual flight trajectory aligns well with existing experimental and numerical studies.

Author

wowefeh830

Language

EN