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|  MIL-C-62207B(AR)
4.6.2 Performance tests.
4.6.2.1 Output voltage. Use items 1, 2 and 5 of table VI or suitable
equipment to determine compliance with 3.3.1.
4.6.3 Environmental tests.
4.6.3.1 Shock.
4.6.3.1.1 Basic design. Use items 3, 4 and 6 of table VI or mount the
assembly in a suitable shock fixture and subject it to the shock test
specified in MIL-STD-81O, 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 conlusion of this test, subject the
assembly to the performance tests of table III.
4.6.3.1.2 High intensity. Use items 3, 4 and 6 of table VI or mount the
assembly in a suitable shock fixture and subject it to the shock test
specified in MIL-STD-81O, 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 III.
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. Use items 4 and 6 of table VI or mount the
assembly in a suitable vibration fixture and subject the assembly to the
vibration test specified in MIL-STD-81O, method 514.2, procedure VIII, except
that the test level shall be the vibration curve shown in figure 1 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 III.
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.
4.6.3.3 High temperature. Use item 7 of table VI or suitable equipment
and subject the assembly to the high temperature test specified in
MIL-STD -810, method 501.1, procedure I. The highest operating temperature
shall be 125F. The performance tests of table III shall be applied.
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