Bizarrely enough alot of those manoeuvres won't cause as much stress as flying fast followed by a roll and pull.
Rate of change of direction will give the G's and the levels of stress produced will be linked to the amount of kinetic energy of the aircraft.
When an aircraft is designed there is normally a large scale computer model built which will run through the manoeuvres of the aircraft generating the loads for each stage of flight and point in the flight envelope. This normally results in excess of 4000 different loadcases. The worst cases for each of the major axes are selected (both linear forces and moments/torsions) then the parts are stressed for those cases. You'll find that there would have been several cases the apply side loads to the radome and that it is fine. The loadcases can sometimes take into account the additional load of a control surface deflection i.e wing bending due to a max rate roll will include the additional forces generated by the aileron moving.
Hope that was clear ... I'm a bit tired and hope I haven't made a technical faux pas.