Project 5,2 ~ In-Flight Participation of a B-52 - lat Lt. F, L. Wiliams OBJECTIVE The objective of this test was to determine the delivery capability of the B52 aircraft, INSTRUMENT ATION Instrumentation of the B-52 for AMPache consisted of 310 yw oscillograph channels which recorded measurements from strain-gage bridges, accelerometers, roll and pitch gyros, radiometers, control position transducers, thermocouples, pressure transducers, and calorimeters, In addition, 14 cameras recoried photo-recorder instmments (14 channels), wing deflection, cloud coverage, and fireball rise and growth, AIRCSAFT POSITION Ik SPACE The following chart shows the airplane's position at zero time and time of shock arrival: Conditions at Time Zero Conmiition at Altitude (Abs ft) 34000 Shock Arrival 34000 Offset (ft} Heading (True-dep) 2ECO lili Q 21 RESULTS Thermal Energy! pee Maximo Temperature: 9 Slant Distance {ft) 38700 Velocity (fps) TAS Ground 740 DELETED 730