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MIL-G-85231 Guided Weapon Control Group Ok-293A/AwwThis specification establishes the design, performance, and acceptance requirements for the OK-293A/AWW Control Group, Guided Weapon, herein after referred to as the control group. The control group consists of Control, Guided Weapon C-9743A/AWW \(Joystick\) and Convertor, Control Signals C-3248A/AWW \(Electronic Package\). The control group is to be located in the aircraft and is to interface with the Guided Weapon Control-Monitor Sets AN/AWW-7B, or AN/AWW-9 \(Pod\) to provide post-launch cockpit control for retargeting and steering of the WALLEYE Data Link Guided Weapon. The control group also provides proportional dc voltage inputs to the AN/ASN-91 computer.

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MIL-G-85231(AS)
3.3.5 Transportability. The control group shall be transportable by air,
rail, truck and ship when mounted in a shipping container as specified in
Section 5.
TABLE I. Dimensions
3.3.6 Nameplates and identification marking. Serial number assignment,
nameplate approval, and identification marking shall be in accordance with
MIL-N-18307.
Identification plates for the joystick
3.3.6.1 Identification plates.
and electronics package shall in accordance with DL 475AS150.
3.3.6.2 Decals, nameplates and markings locations. All decals,
namepleates, and markings shall be affixed to the control group in accordance
with DL 475AS150.
3.3.6.3 Serial numbers.
Serial numbers will be assigned by the procuring
activity for the control group specified in the contract or purchase order.
The contractor shall serialize sequentially all control groups which are
specified in the contract.
3.3.7 Color and finish. Color and finish of the control group shall be
in accordance with DL 475AS150 and MIL-E-5400
The generation of electromagnetic
3.3.8 Interference control.
interference by the control group and the vulnerability of the control group
to electromagnetic interference shall be controlled within the limits of
MIL-STD-461 for CLass A1 equipment. EMI testing shall be accomplished under
standard conditions specified in 3.3.10 and in accordance with the procedures
of MIL-STD-462 to demonstrate compliance with the MIL-STD-461.
3.3.9 Safety. Safety requirements shall be in accordance with
MIL-E-5400.
3.3.9.1 Human performance/Human engineering. The control group and all
component parts thereof, shall be designed in accordance with MIL-STD-1472.
Recognized principles of human engineering as specified in MIL-H-46855 shall
be followed during design.
3.3.10 Standard conditions. The following conditions shall be used to
establish normal performance characteristics under standard conditions and for
making laboratory bench tests.
Temperature
Room ambient (25 ±5°C)
a.
Normal ground
Altitude
b.
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