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This is a vertical take-off and landing fighter corresponding to the sixth generation in terms of thrust-to-weight ratio. Based on the engine "izd.30". Thrust-to-weight ratio at maximum take-off weight is equal to one. With a normal take-off weight, the fighter will take off vertically at any ambient temperature.I did not count on centering for this project, I hope the heavy nose is balanced by an equally heavy tail section
This is a vertical take-off and landing fighter corresponding to the sixth generation in terms of thrust-to-weight ratio. Based on the engine "izd.30". Thrust-to-weight ratio at maximum take-off weight is equal to one. With a normal take-off weight, the fighter will take off vertically at any ambient temperature.
I did not count on centering for this project, I hope the heavy nose is balanced by an equally heavy tail section
