Has anyone done 30+ G/s of centripetal acceleration in a banked turn?

I'm currently designing a UAV with aerodynamic boundary active flow control (coflow jets). I expect to achieve a Cl of up to 1.8. With a 1 m2 wing area, and 5:1 aspect ratio. I should be able to sustain up to 60 G turns @ 410 km/h. The alpha should be around up to 20 degrees before stall @ 9x10⁶ Re

I'm seeking some advice on how to correctly reinforce the airframe. Currently I'm using cross weaved CFRP tubing for the spar, and CFRP sheets for the ribs. This should theoretically sustain 30 Gs without any issue, but my battery, engine, and ESC will probably shear through the fuselage.

I appreciate any ideas.