John Company

Department of the Air Force Report, 1996

DOW-UAP-D048 · page 70 of 181

Page 70 of 181 of DOW-UAP-D048

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6.3.1 Optimum Mode-5 Shaping Constants
The percentage of Delta vehicles that break up during simulated random-attitude turns
are plotted against failure time in Figure 23. The same breakup qa's used in the
Atlas IIAS calculations were used here. It can be seen from the figure that over 50% of
the vehicles break up, either immediately or eventually, if a turn begins between about
10 and 115 seconds.
100
90
80
-
70
-
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60
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Q)
50
a..
a.
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40
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ffl
Q)
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cc
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20
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0
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, /1 \ , :
i
: Delta-GEM:
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1:
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q-alpha in deg-lb/tt
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,:
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--+ q-alptla = 5,000
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·················!····················f····················f····················f···················1.... , ___: ---1
0
40
80
120
160
200
240
280
Failure Time (sec)
Figure 23. Delta-GEM Breakup Percentages
9/10/96
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