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What is the relationship between the rotating diameter of model helicopter propeller and engine power and aircraft weight?
Generally speaking, the model rotorcraft is inefficient. We calculate according to three times the power required by a fixed wing (trainer) with the same weight:

It weighs about 3KG.

What is the minimum power required by the engine? How should I calculate it? Can a friend explain it to me? Thank you very much.

A 3KG fixed-wing trainer needs about 150W power to barely take off and keep flying horizontally.

The rotorcraft needs to be multiplied by 3 to get 450W W W.

If a 4S lithium battery is used, the current will be nearly 30A according to 16V.

This kind of relatively large brushless motor is very abundant on Taobao and easy to find.