MIL-G-85742-5 Guidance Control Section, Guided Missile Servo SectionThis specification sheet establishes the performance and test requirements for the servo section used in the Guidance Control Section of the SIDEARM Missile.

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MIL-G-85742/5(AS)

TABLE I. Telemetry and aircraft signal line resistance.

4.2.2.1 Gas generator squib resistance. Measure squib resistance be-

tween pins 22 and 31 on connector A3A1J1 to determine conformance to 3.2.1.2

using a test current of less than 5 milliamperes.

4.2.2.2 Input voltages (pre-PCO). The input ac voltage applied at pin

34 with return at pin 11 of A3A1J1, shall meet the requirements of

3.2.1.3.1. The input dc voltage applied to pin 17 of A3A1J1 shall meet the

requirments of 3.2.1.3.2.