MIL-DTL-83502E
4.8.10 Vibration (see 3.13). Sockets shall be tested in accordance with test procedure EIA 364-28.
The following details shall apply:
a. Test condition - III.
c.
Following the test, contact resistance and contact withdrawal force shall be measured in
4.8.11 Shock (specified pulse) (see 3.14). The socket shall be tested in accordance with test procedure
EIA 364-27. The following details shall apply:
a. Mounting method and detection circuit - Mounted by normal means monitoring equipment used
shall be capable of detecting circuit interruptions greater than 1 microsecond.
b. Preparation - Mated with a test plug (see figure 2).
c. Test setup: See figure 5.
d. Acceleration requirements - Test condition G.
e. Number of blows - One blow in both directions along each of three mutually perpendicular axes for
a total of six shocks.
APPLICABLE TEST PLUG W ITH
LEADS MATED W ITH SOCKET
APPLY ONE LEAD OF DC POW ER
SUPPLY OR MONITORING EQUIPMENT
SOCKET UNDER TEST
SOCKET TO BE SECURED TO
RESPECTIVE SHOCK OR
VIBRATION FIXTURE
SOLDER JOINT OR W ELD TYP
CONNECTIONS CONTACTS W IRED
SERIES TO ESTABLISH SERIES CIRCUIT
APPLY ONE LEAD OF DC
POW ER SUPPLY OR
MONITORING EQUIPMENT
FIGURE 5. Vibration and shock test setup.
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