TABLE 6.2
DATA SUMMARY, B-56
Shot
Radient Exposure, cal/om:*t
1
2
4
5
478
36.2
17.4
45.9
—
_
1.2
3.7
5.2
62
Max Irradiance, cal/om’-seet
6*
Max Temperature Rise of Elevator Skin
at Station 144.8, pexyent of 400 F limit
652{
45
37
“4
~~
Max Overpreassure, pal
Max Pressure, psi, en underaide of:
Wing
Puselage
Stabilizer
0.81
0.56
0.42
0.60
0.22
0.90
0.82
1.20
0.62
0.64
0.88
0.48
0.48
0.60
0.68
0.67
0.88
0.27
0.23
0.25
Stabilizer, Station 62
89
60
37
18
27
Fuselage, Station 1476
Wing, Station 1062
50 to 70
50
47 to 67
50
22 to 42
44
67 to 87
83
4 to 20
49
Max Positive Bending Moments, §
percent of linit?:
* Bead-on orientation.
tAverage of multiple instrumentation.
t Temp-tape data.
$ Max positive bending moments are the peak incremental bending plus dead weight and in-flight
conditions.
{Bending moment limits are defined as two thirds the static test ultimate.
TABLE 6.3
DATA SUMMARY, B-<7
Shot 3 data unusable because of low yieid. No participation in Shot 5.
Shot
1
2
4
6
Radiant Exposure, * cal/cm*
$2.1
17.6
16.3
11.8
Max Irradiance, * cal/om*-sec
§.27
2.67
4.10
8.33
‘1.33
Time to Peak Irradiance, seconds
3.81
3.24
2.41
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
6.0
Time to Shock Arrival (Station 1217), seconds
110.5
169.1
116.9
73.66
Peak Overpressure, psi
0.31
0.22
0.26
0.26
Peak c.g. Acceleration, g's
0.38
0.32
0.28
_
* Corrected to zero incident angle.
77