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|  MIL-T-81734D(AS)
3.2 Design and construction. The Airborne Weapon Control System Test
Set AN/AWM-23(V) shall consist of the items of Table I. Each of the
items of Table I shall include all necessary cables required for operation.
3.2.1 Design features. Except as otherwise specified herein, the de-
sign and construction o-f the test set shall be in accordance with MIL-T-21200.
3.2.1.1 Method of operation. The items of Table I shall be operable in
manua1, semiautomatic, or automatic modes as specified in the applicable
specification.
3.2.1.2 Commercial test equipment. Commercial test equipment installed
in the test set shall meet the functional requirements of the test set.
The test set, including commercial test equipment installed in the test set,
shall meet the environmental requirements of 3.2.3.2.
3.2.1.2.1 Other commercial components. Other commercial components
(such as power supplies, tape readers, or tape recorders), may be incorp-
orated in the test set. When installed in the test set, they shall meet
the environmental and electrical service conditions of this specification.
3.2.1.3 Circuit grounds. To the greatest extent practicable, circuit
ground or common shall be connected to the chassis, enclosure, or ship's
hull at only one physical point. The ship's hull shall not be used as
an electrical conductor in equipment circuitry.
3.2.1.4 Interchangeability. Interchangeability shall be in accordance
with MIL-STD-454, Requirement 7.
MIL-T-21200 shall apply.
3.2.1.5 Identification of product.
3.2.1.6 Human factors. The human engineering requirements of MIL-STD-
454, Requirement 62, shall apply.
3.2.1.7 Test set generated acoustic noise. The equipment acoustic
noise requirements of MIL-T-21200 shall apply except that liquid cooler
noise level shall not exceed 80 decibels in any octave to 9600 Hertz (Hz),
at a distance of 3 feet.
cooling.
Forced-liquid
Liquid coolant shall be routed within
3.2.1.8
the Low Frequency Test Station, the Radio Frequency Test Station and the
Fill-Drain Stand as required. Flow/no flow indication of liquid coolant
shall be provided in these test stations. Individual flow rate require-
ments for each test station shall be as specified in the applicable
specification. Maximum liquid coolant flow rate shall be 13 gallons per
minute (gpm).
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