= ys 366 (MOHAWK ) Project 5.3 - In-Plight Participation ef « B-66B - R. W. Bachman OBJECTIVE The primary objective of this t was to measure the guet and bigh Q field effects of low altitude flight. weapon on a B-66B aircraft ¥ , BEST AV AILABLE coP TESTRIMEFTATION Instrumentation on the B-66B for this shot consisted of the following: 67 strain gages at 5 stations and 26 T.C, at 7 stations on the L.H. wing; 16 strain gages at 1 station and 6 T.C. at 2 stations om the R.A. wings 2% otrain gages at 4 stations and 12 7.C. at 2 stations om the L.A. hori- sontal stabiliser; 9 strain garee at 1 station and 2 T.C. at 1 station on the R.H, borisontal stabiliser; 3 strain gages at 1 station end 9 T.C. at 4 stations on the L.H. elevator; 2 strain gages at 1 station and 6 T.C. at 1 station on the A.M. elewator; 24 1.C. at 9 etations on the fuselage; 26 channels of engine information; ? pressure plokupe on the wing; 3 pressure Pickupe om the empennage; and 9 pressure pickupe op the ‘uselage; 17 accelerometers on the fuselage, empennage and nacelle; 1¢ oalorimetera and 2 radiometere in the tail; 3 calorimeters in the fuselage belly; wing and tail deflection cameras; 32 basic aircraft flight instruments on a photo recorter panel; and & channels of correlation date. POSITION Using the K-5 radar system, the B-€6B vas positioned at an altitude of 6,000 feet, on a heating of 050 derrees, and a borisontal range of 12,700 feet at time serc, At time of shock arrival, the horisontal range was 28,400 fect, with the aircraft on the same beading and at the sane altitude as before, - 36 = 36