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| MIL-G-85299(AS)
on the STRAY ENERGY GO/NO-GO lamps until both an acceptable
input is monitored, and the latch has been reset by the PRESS
TO READ DVM/RESET push-button or by changing the position of
the FUNCTION SELECT switch.
The output signal shall be as specified
(9) Missile audio, W1, P2-15.
in 3.4.5.2.a.(10)
FUNCTION SELECT test three.
c.
This input function shall be as specified
(1) Launch latch, W1, P2-3.
in 3.4.5.2.b.(1).
This input function shall be as
(2) Power changeover, W1, P2-19.
specified in 3.4.5.2.b.(2).
(3) Motor fire squib, W1, aft strike contact.
(a) A 0.97 + 5 percent ohm resistive load shall be applied between
ground and the aft striker contact for 20 milliseconds out of
each second. The load pulses for the motor fire squib shall
be applied simultaneously with those for the launch latch and
power changeover inputs.
(b) The input pin shall monitored for correct voltage in
accordance with the accept/reject limits as specified in table
III. The accept/reject decision shall be updated at a one
Hertz rate, at a point 14 milliseconds after application of
the 20 millisecond resistive load pulse.
(4) Missile filament, W1, P2-22, 25.2 volts dc. The test set shall
provide a direct switched current path from the input pin W1,
P2-22 to auxiliary fire output pin, W1, P2-27. Resistance of the
circuit path shall be not greater than one ohm.
(5) Auxiliary Fire, W1, P2-27.
(a) The test set shall provide a direct circuit path as specified
in 3.4.5.2.c.(4)
(b) The external load shall be not less than 950 ohms.
Performance shall be as specified in
(6) Electrical cage, W1, P2-30.
3.4.5.2.b.(6).
(7) Electrical cage return, W1, P2-23. Performance shall be as
specified in 3.4.5.2.b.(7).
Performance shall be as specified in
(8) Missile audio, W1, P2-15.
3.4.5.2.a.(10).
d.
FUNCTION SELECT test four.
(1) Left-right reference, W1, P2-34.
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