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MIL-G-85299(AS)
(2) Master arm, W1, P2-20 (W2, P2-6).
(a) A 13.0
5 percent ohms resistive load shall be applied
between ground and input pin W1, P2-20 for 20 milliseconds out
of each second.  The master arm load pulse shall be applied
simultaneously with the 28 volt BUS load pulse of
3.4.5.3.a.(1)(a).
(b) The input pin shall be monitored for correct voltage as
specified in 3.4.5.3.a(1)(b).
(c) Capacitance from pin W1, P2-20 to ground shall be not greater
than 1.2
(3) Cool control, W1, P2-12 (W2, P2-20).
(a) A 200
5 percent ohms resistive load shall be continuously
applied between ground and input pin W1, P2-12.
(b) The input pin shall be monitored for correct voltage in
accordance with the accept/reject limits of table IV.
(4) 115 v, 400 Hz, phase A, W1, P2-1 (W2, P2-9).
(a) A 98K ohms minimum resistive load shall be continuously
applied between ground and input pin W1, P2-1.
(b) The input pin shall be monitored for correct voltage in
accordance with the accept/reject limits of table IV.
(5) Ground, W1, P2-9 (W2, P2-16).
(a) Continuity test shall be conducted to the power ground pin,
W1, P2-21 (W2, P2-18). Accept/reject limits: accept for not
greater than 800 ohms; reject for greater than 2,500 ohms.
Accept/reject decision shall be updated at a one Hertz rate
simultaneously with the updating of the signals of
3.4.5.3.a.(1) through (4).
(6) Fire signal, W1, P2-13 (W2, P2-1).
(a) A 1.5
5 percent ohms resistive load, fused with a 1.5 ampere
slowblow fuse, shall be continuously applied from ground to
pin W1, P2-13.
(b) The input pin shall be continuously monitored for a stray
energy accept/reject decision as specified in
3.4.5.2.a.(7)(b).
The requirements are as
(7) Missile audio, W1, P2-15 (W2, P2-19).
specified in 3.4.5.2.a.(10).
b.
FUNCTION SELECT test two.
The requirements are as
(1) Fire signal, W1, P2-13 (W2, P2-1).
specified in 3.4.5.2.b.(3).

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