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|  MIL-C-48610B(AR)
4.6.2.2 Output voltage characteristics. Use item 1 of table VIII or
suitable equipment to determine compliance with 3.3.2.
4.6.2.3 15 volt sense and overcurrent. Use item 1 of table VIII or
suitable equipment to determine compliance with 3.3.3.
4.6.2.4 Q-switch drive. Use item 1 of table VIII or suitable equipment
to determine compliance with 3.3.4.
4.6.2.5 Sync signals A and B. Use item 1 of table VIII or suitable
equipment to determine compliance with 3.3.5.
4.6.2.6 Q-switch drive regulator. Use item 1 of table VIII or suitable
equipment to determine compliance with 3.3.6.
4.6.3 Environmental tests.
4.6.3.1 Shock.
4.6.3.1.1 Basic design. Mount the assembly in a suitable shock fixture
and subject it to the shock test specified in MIL-STD-810, method 516.2,
procedure I, figure 516.2-2. Apply three half sine wave shock pulses in each
direction along the three axes. Peak amplitude shall be 40 4 g with a time
duration of 18 3 msec measured at the 10 percent amplitude points. At the
conclusion of this test, subject the assembly to the performance tests of
table V.
4.6.3.1.2 High intensity. Mount the assembly in a suitable shock fixture
and subject it to the shock test specified in MIL-STD-810, method 516.2,
procedure IV, figure 516.2-2. Apply three half sine wave shock pulses in each
direction along the three axes. Peak amplitude shall be 100.0 10.0 g with a
time duration of 1.5 0.2 msec measured at the 10 percent amplitude points.
At the conclusion of this test, subject the assembly to the performance tests
of table V.
4.6.3.2 Vibration. Vibration A as specified in 4.6.3.2.1 shall be
conducted only for first article inspection. Vibration B as specified in
4.6.3.2.2 shall be conducted only for quality conformance inspection.
4.6.3.2.1 Vibration A. Mount the assembly in a suitable vibration
fixture and subject the assembly to the vibration test specified in
MIL-STD-810, method 514.2 procedure VIII, except that the test level shall be
the vibration curve shown in figure 4 and duration of exposure shall be not
less than 80 minutes per axis. At the conclusion of this test, subject the
assembly to the performance tests of table V.
4.6.3.2.2 Vibration B. This test shall be conducted as in 4.6.3.2.1
except that the period of vibration shall be not less than 15 minutes in each
axis.
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