= 4 196 (Tea) Project 5.3 - In-Flight Participation of a B-O6B - R. W. Bachnen OBJECTIVE The of a " AuSTmUNTArioN objective of this test was to measure the gust effects nuclear device on a 8-668 airereft in flight. wr Instrmmentation on the B-66B ron200) consisted of the following: 67 atrein gages at 5 atations and 26 thermocouples at 7 stations on the left hand wing, 16 strain gages at ] station and 6 thermocouples at 2 stations on the right hand wing, 25 strain gages at 4 stations and 12 thermocouples at 2 statians op the left hand borisontal stabiliser, 9 strain gages et 1 station and 2 thermocouples at 1 station on the right hand torisontel stabiliser, 3 strain gages et 1 station and 9 thermocouples at 3 stations on the left hand elevator, 2 strein gages at 1 station and 6 thermocouples at 1 station on the right hand elevator, 24 theracecuples at 9 stations on the fuselage, 20 channels of engine information, 3 pressure pickups on ving, 3 pressure pickups op empenage and 9 pressure pickups on the fuselage, 17 accelercaeters on the fuselage, empenage snd nacelle, lo oslorizeters acd 2 redioneters in the tail and 3 calorimeters in the fuselage belly, wing and tail deflection cameras, 32 vasic sircraft flight inetruments on a photo recorder pane) and 8 eorrelation obannels. POS1Ti0N The K-5 Radar system was used to position the airoreft, At H - 1130 minutes the navigstor indicated a 5 second late position and the aircraft was obliged to abort the mission. @ BEST AVAILABLE COPY -_.w-