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I'm wondering about theoretical maximum velocities of supersonic electric aircraft. I think the fastest demonstration of any type of aircraft has been close to mach 10. This was done using a rocket engine, so propulsion would not be limited by air characteristics as much as a fan's propulsion would (I think).
Under best conditions; Assuming an incredibly high power to weight ratio of motors, extremely aerodynamic design, strongest materials, etc.
Theoretically, does anyone know what the limiting factors in the velocity of an electric fan propelled supersonic aircraft would be (barring energy use)? Does it depend on size, etc?
Could it reach mach 2+?
Thanks a lot in advance for any input.
EDIT: Please see question change below
Under best conditions; Assuming an incredibly high power to weight ratio of motors, extremely aerodynamic design, strongest materials, etc.
Theoretically, does anyone know what the limiting factors in the velocity of an electric fan propelled supersonic aircraft would be (barring energy use)? Does it depend on size, etc?
Could it reach mach 2+?
Thanks a lot in advance for any input.
EDIT: Please see question change below
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