I figured you were using Orbiter.
I honestly don't know the tolerances of the component in question. As a point of reference... in fact the only point of reference I can think of for what you are doing would be the Apollo CSM. Its maximum main engine thrust was 91,000 N of thrust (or 91kN) and it was capable of using that thrust while docked to the LEM.
So I think it is feasible as far as compression goes, shear I have no clue since Apollo was stacked in a strait line not and L or + shape.
Must resist urge to download Orbiter again... must work on LWAMI 3.11...