Project 5.5 - In-Flight Participation of F-B84F Aircraft - Lt, J. A. Sabatella OBIECTIVE Waiter (Capabilities F-84F) - This participation was an attempt to determine the capability of the F-84F aircraft by subjecting it to both thermal and symmetric blast loads, Barley (Sideloads F-84F) - The object of this participation was to study the dynamic response of fighter structures to anti-symmetric blast loads, IXSTRUMENTATICN . Waiter - 100 data channels were available to record moment, shear, : and torsion loads; accelerations; overpressure; temperatures thermal strain; and aircraft attitude, recorded, All of these channels were succesefully However, a flap camera failed to operate properly, Barley - 100 data channels were available to record easentially the same information as above, Out of these 100 channels, there was only one channel that failed, AIRCRAFT TOSITION IN SPACE Walter - At time zero, the aircraft was flying at an altitude of 31,614 ft on an inbound heading of 070°, The horizontal range was 18,614 ft with a left offset of 246 ft, The shock arrival position DELETED “°* 31,217 ft altitude, to the right, DELETED DELETED ‘and 1,760 ft offset The true air speed waa 800 fps, Barley - At time zero, the aircraft was flying at an altituwie of 35,(49 ft on an Inbound hending of 060°, The horizontal range and offset were -26,973 ft and 34,808 ft respectively, -21- gm At shock arrival DELETED SNL A\