MIL-PRF-39015E
4.8.10 Torque (see 3.16).
4.8.10.1 Operating (see 3.16.1). The maximum operating torque required to move the contact arm on
the resistive element shall be determined at approximately 10 percent, 50 percent, and 90 percent of the
actual effective electrical travel by the torque wrench or by any other method acceptable to the
government.
4.8.10.2 Clutch (see 3.16.2). The contact arm shall be adjusted to each extreme limit of mechanical
travel, and sufficient torque shall be applied to the lead screw actuator to permit the contact arm to idle for
25 complete mechanical turns of the lead screw actuator. During idle, an electrical indicating device
connected between the contact arm terminal and the adjacent end terminal shall be observed for
electrical continuity. After idle, the lead screw actuator shall be rotated in the opposite direction and the
indicating device observed to determine if the contact arm reversed direction without ohmmeter
discontinuity.
MIL-STD-202. The following details and exceptions shall apply:
a. Test condition: B.
b. Measurement before cycling: Total resistance and setting stability shall be measured as specified
c. Measurements after cycling: Setting stability, total resistance, and continuity shall be measured as
d. Examination after test: Resistors shall be examined for evidence of mechanical damage.
4.8.11.1 Setting stability. The contact arm shall be set at approximately 40 percent of the actual
effective electrical travel. An adequate dc test potential shall be applied between end terminals. The
voltage between the end terminals, and the voltage between one end terminal and the contact arm, shall
be measured and applied to the following formula:
Setting stability = E1 x 100
(in percent)
E2
where:
E1 = Voltage across one end terminal and the contact arm terminal.
E2 = Voltage across the end terminals.
The difference between the initial measurement made before the environmental test and the
measurement made after the test indicates the setting stability in percent.
4.8.12 Solderability (applicable to terminals P, W, X, and Y) (see 3.18). Resistors shall be tested in
25
For Parts Inquires call Parts Hangar, Inc (727) 493-0744
© Copyright 2015 Integrated Publishing, Inc.
A Service Disabled Veteran Owned Small Business