Nav Gain Assembly used in the Guidance Control Section of the SIDEARM Missile.

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MIL-G-85742/4(AS)

4.2.3.6 Navigation gain function. Initialize the unit in the position

shown in Figure 1. Ground the Nav Gain Set line and apply 10 V to the

GB/NG input disable line. Measure the Magamp In outputs and remove the 10 V

from the GB/NG input disable line. The outputs shall meet the require-

ments of 3.2.6.

Preparing activity

Navy-AS

(Project 1420-NO4)