ou
to flight time; one accelerometer was unreadable due to defocusing cf
its galwanometer ani one calorimeter, although functioning properly,
was not considered reliable jue to its large range ani omall deflection.
Three or four thermocouples my have been ~alfunctioning but, due to
the small temperature rises existing, it was impossible to definitely
deternine.
"xcessive vibration of the photo panel again occurred at
shock arrival, rendering two frames (.125 sec) unreadable.
All 26
gages functionat properly and no date was lost.
Gust Data:
The aircraft experienced a multiple shook arrival
imiteating that it was aren ye triple point path,
“‘werpresasure
Measuned was about m.- the first shock, about half that on the
secomi shock 1.6 seconds lates, and half again om a@ third shock .25
seconis late.
Gust resronse vas about 75% for torque an? 406 for
shear and benting, eomfirwineg the load iistribution encounteret on
) ACPOSST),
Future positions will be revised to account for
SEha nev Inai distribution.
Therm) Data:
expected,
A
7herml response was again considerably less than
T of about 30°F was experierncet om the honeycomt surfaces.
Muclear Radiation:
A reading __ taken from the pilots
thin a predicted
\
based on positioning yield,
General: “The participation was again successful from this pro
ject's standpoint.
Gust resr<ses vere ganeral’y higher than creviously
experianced ami the data collected has thie far cormelate? evcellently
with previous data ani predtctiona,
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