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An odd question

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Whilst I understand the hang test to get the angle of dangle and back tilt, how do you establish the vertical component to get a CG point on a paramotor ?

The reason I ask is that with a gyro having the motor thrust in line with the cg is desirable in preventing some nasty things happening although the separation in distance of the drag component(wing/rotor) is quite large in comparison or am I asking a pointless question



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