aay A RESULTS Thermal: The temperature rise was insignificant due to the limiting side loads position and very small thermal inputs that were received. Gust: At time of shock arrival the gust load was 48% of limit wing bending at station 493.0, 45% at station 615.0 and 42% at station 144.0, Since the fuselage bending, shear and torsion pages were added only recently, they have not been calibrated, and results from recorded inputs cannot be compared to limiting criteria at this time, However, it is believed that the recorded fuselage inputs for this event were small, Overpressure: DISCUSSION The calibration of the side loads gages in the fuselage will not be accomplished until return to the ZI, Therefore the percent bending in the fuselage will not be known until the calibration is completed and the data reduced, 4) .ac . . oa ee ithe go, - 33 -