John Company

Department of the Air Force Report, 1996

DOW-UAP-D048 · page 49 of 181

Page 49 of 181 of DOW-UAP-D048

Text

A machine read this text from the scan. When the text and the image disagree, the image is right.

9/10/96
[
1
Atlas IIAS Impacts
Random-Attitude Failures at 130 sec.
Thrust to 280 sec,
Breakup q-alpha = 5,000 deg-lb/ft2
40
Figure 8. Atlas IIAS Impacts with Breakup
RTI