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What is the lift coefficient of an Antonov An-225?

Anonymous

∙ 14y ago

Updated: 9/19/2023

The lift/drag coefficient of an Antonov An 225 is 19 with no change in the aerodynamics,Mach 4 mark,cruising altitude with the nett thrust payload of max.600 tonnes.

Um more like 4.273 which is the inverse of the Thrust. Max load 200 ton, and a service ceiling of 11,000m

Wiki User

∙ 14y ago

What else can I help you with?

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