b.
c.
d.
e.
f.

Bombing Equipment, Optical Sight
Aerial Mapping Camera
Radar Tracking from Ground
Station Keeping, Radar
Optical Ground Tracking

In the radar navigation method, the aircraft radar is used to

determine the slant range distance to various targets placed at know

locations in the test area. Knowing aircraft altitude, it is possible
to calculate rosition using the above slant range data. Tata recording
was accomplished by means of radar scope photos.

with the optical bomb sight, visual sightings are made on land-

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marks or targets indicated on a chart and the aircraft position calculated.

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The aerlal mapping camera is activated shortly before time
zero anc operates through detonation tice until the film is exhausted.
The exact tire of each photographic exsosure was recorded by the oscillograph. If the aircraft flies over terrain having some recognizable

features, it would oe possible from scrutiny of the aerial photographs
to chart the course of the aircraft as a function of time and determine
its locztion at zero time.
The slant ranre anc azimuth data from ground based radar track~
ine ecuirpment can ce used to determine aircraft location. This equipment

also gives an approximate altituce figure and was used primarily for
monitoring purroses to determine that aircraft would not be in a danger

rezion at burst time or shock arrival.
"Oration keeping” is the rethod whereby an aircraft is posi-

tioned ty maintainine a fixed positicn with respect to another airborne
zircraft, in tni: instance the "drop" aircraft. The two aircraft fly
at constant, thou,hn rossiply different, aititudes. If the difference
in &ititude is Known, then the rosition of the test aircraft can be ex-

pressed in terms of a cearin: ard slant rance to the "drop" aircraft.

The correct cearing and slant ranre is maintained by use of radar.

Two-station optical rround trecking can be used to determine

aircraft position if altitude is mown. Cperatior derernds unon measuring
the azimuth and elevation angles from the try ground stations to the aircraft as a function of tine. Exact loc.tion of ground stations must be

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2.3.2

Fesronse Measurements

Aircraft reaction to clast loadin: was measured in terms of acceleration, shear, torsion, and cCenainr response at various points on
the structure. The sensin.: elements or devices used for these measurements in all instarces emrloyed the strain eaze rrincirle, which makes
use of the fact that the resista:ce of a wire varies in direct proportion

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are made of esrecially comrounded wire thet can te either pdor.sed to a

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to its elongation within the elastic limits of the wire.

Strain gages

part of a structure or stretcne: cetween two objects that move relative
to each other. Tne former apriicaticn is senerally used when measuring
tne strain in a structural remcer, tne latter apriication, the unbonded
strain cave,

te,

as

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is cenerally emrloyed in .cesific sernsinre devices such as

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