1.1.3
Power comprising 28 volts d.c, at ten amps, and 110
volt. oO cycle a.c. at 5 amps should be available
to operate relays, butterfly valves and sample radiation
monitoring equipment which will be used with the filter
unit, Suitable wiring to the filter unit will be
required,
1.1.4
Depending upon the configuration of the aircraft used
and clearances between the wing and the ground, the
filter unit may be mounted either on the wingtips or
on pylon position underneath the wings. Ordinarily
it would be desirable for an aircraft to carry two
filter units,
1.2
Gas Samples:
1.2.1
Snap-type Samples.
1.2.1.1 The polyethelene bag snap-type equipment will be
required and should have a capacity of 15 to 100
cubic feet at the sampling altitude,
The auxiliary
power requirements should be negligible, but wiring
will be required to carry power for the relay valves
opening and closing the bag.
1.2.1.2 This equipment should be located in a space within
the fuselage of the aircraft,
An external air
sampling probe leading to the sampling apparatus
will be required,
1.2.2
Pressure-bottle Type:
1.2.2.1 It is anticipated that a pressure-bottle type of
gas-sampling apparatus similar to that being
developed for the F-8lG's will be required as
an alternative to the bag type.
The physical size
and power requirements for this type of apparatus
will be similar to those for the system being
designed for the F-8)G,
1.2.2.2 This apparatus should be installed in suitable space
within the fuselage of the aircraft and will require
an external sampling probe.
Desired Sampling Altitudes:
2.1
The desired sampling altitude will depend upon the
yield of the detonation and the burst height but,
216
SWEH -2-003);
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oP
AFWL/HO