to flight time; one accelerometer was unreadable due to defocusing of
its galvanometer and one calorimeter, although functioning properly,
was not considered reliable due to its large range and small deflection.
Three or four thermocouples may have been malfunctioning but, due to
the small temperature rises existing, it was impossible to definitely
:
determine.
Excessive vibration of the photo panel again occurred at
- shock arrival, rendering two frames (.125 sec) unreadable.
All 26
gages functioned properly and no data was lost.
Gust Data:
The aircraft experienced a multiple shock arrival
indicating that it was above the triple point path.
Overpressure
measured was about SEER on the first shock, about half that on the
second shock (AE 16ter, and half again on a third shock Page?
seconds later.
Gust response was abouttor torque and
yy
or
q
shear and benling, confirming the load distribution encountered on
(LACROSSE).
Future positions will be revised to account for
the new loaj distribution.
Thermal Data:
expected.
A
Thermal response was again considerably less than
T of about 30°F was experienced on the honeycomb surfaces.
~~)
Nuclear Radiation:
cp
uy
A reading of
was taken from the pilots
film badge. pe «:: predicted based on positioning yield.
General:
The participation was again successful from this pro-
ject's standpoint,
Gust responses were generally higher than previously
experienced and the data collected has thus far correlated excellently
with previous data and predictions.
COPIED/DOE
IANLRG we,