302
’
"
.
a
903
Maa
6
WE, Lewin
Damage:
There vee no spparent damage to the aircraft,
Instrunentation:
There was no apparent damage to the instrumentation,
Of the 50 oscillograph recorded parsmeters, 47 produced usable data,
a
thermocouples gave unreliable readings.
moclear
no trace vas recorded,
One shear gage was disconnected and
One of the blast oamers
pictures was unintellircible
due to muddy water splashed on the lens during takeoff.
fe
Two
The photopeanel
camera, recording 26 parsmeters, functioned properly and produced good data.
It vibrated at shock errival but no date was lost,
Quast Data:
‘
The aircraft experienced a double shock arrive) indicating
t
that it waa above the triple point path.
s strein
on the first shook, and about 1/3 thet on the second shock 0,84 seconds later.
-oraft
Gust response was about 15% for sheer and bending and about 25% for torque on
rae
.
lear
.
oie
the first shook.
Therwal Data:
Overpressure measured about
Gust response vas negligible on the second shock.
Although not of primary importance, thermal response was
agein considersbly less than predicted.
& OT of about & F on the unpainted
and about 12° F on the bleck painted honeycomb was recorded.
Wacleer Radiation:
ding
t the
file bedge.
General:
ock
etendpoint.
t.
measured.
A reading of 1,6 REM wae recorded on the pilot's
Based on positioning yield, 3.454 REM vas predicted.
The participation was again sucesssful from thie project's
I+ produced data in the lower yield range not heretofore
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