l4y at” DELETEN '(PAKOTA) Project 5.5 = In-Flight Participation of FeS4F Aircraft - Lt R. F,. Mitchell Lt J. A. Sabatella Objective Waiter (Capabilities F-84F) - This participation was an attempt to determine the capability of the F~S4F aircraft by subjecting it to both thermal and symmetric blast loads, Barley (Sideloads F-84F) = The objective of this participation was to study the dynamic response of fighter structures to anti-symmetric blast loads, Instrumentation Waiter = 100 data channels were available to record moment, shear, and torsion loads; accelerations; overpressure; temperature; thermal strain; and aircraft attitude. All of the chamels were successfully recorded, Barley = Out of the 100 channels available torecord essentially the same information as above, there were 5 channels that failed. In add- ition, the two fireball cameras were inoperative. Aircraft Position in Space Waiter = At time zero, the aircraft was flying at an altitude of DELETED ft and zero offset, DELETED The shock arrival position horizontal range, and zero offset, DELETED DELETED DELETED Barley — At time zero, the aircraft was flying at an altitude of DELETED were cOprEDIDOE oot RG DELETED '\ The horizontal range and offset 'yespectively. - 26 - At shock arrival pELETED