TABLE 6.2 DATA SUMMARY, B-36 Shot Radient Exposure, cal/em't 1 2 4 5 6* Max irradiance, cal/om'-seet 62 478 35.2 17.4 45.9 _ Max Temperature Rise of Elevater Skin 62 45 37 “ ~ Max Overpreseure, pal Max Pressure, pai, ew unteraide of: 0.81 0.56 0.42 0.60 0.22 Wing 0.90 0.62 0.48 0.68 0.27 Stabilizer 1.20 0.83 0.60 6.86 0.25 at Station 144.8, pareent of 400 F limit Fuselage 0.92 0.64 0.48 —~ 1.2 3.7 5.2 0.67 0.28 Max Positive Bending Moments, § percent of Limit#: Stabilizer, Station 62 59 60 37 18 27 Fuselage, Station 1476 Wing, Station 1062 50 to 70 5&0 47 to 87 50 22 ta 42 44 67 to 87 63 4 to 20 49 * Head-on orientation. t Average of multiple instrumentation. { Temp-tape data. § Max positive bending moments are the peak incremental bending plus dead weight and in-flight conditions. TBending moment limits are defined as two thirds the static test ultimate. TABLE 6.3 DATA SUMMARY, B-47 Shot 3 data unusable because of low yield. No participation in Shot 5. Shot 1 2 4 6 Radiant Exposure, * cal/cm* 32.1 17.5 16.3 11.8 Max Irradiance, * cal/om*-sec 6.27 2.67 4.10 5.33 Time to Peak Irradiance, seconds 3.81 3.24 2.41 1.33 Duration of Irradiance, seconds 48 46 33 12 Peak Temperature Right Stabilizer, F 134 44 81 99 Time to Peak Right Stabilizer Temperature, seconds 9.0 10.0 7.0 5.0 Time to Shock Arrival (Station 1217), seconds 110.5 189.2 116.9 73.66 Peak Overpressure, psi 0.31 0.22 0.26 0.25 Peak c.g. Acceleration, g's 0.38 0.32 0.28 _ * Corrected to zero incident angle. 77