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|  MIL-T-48460B(AR)
4.6.2 Performance tests.
4.6.2.1 Output voltage linearity. Use item 1 of table VI to verify com-
pliance with the requirements of 3.3.1.
4.6.2.2 Output voltage ripple. Use item 1 of table VI to verify compli-
ance with the requirements of 3.3.2.
4.6.2.3 Rest output. Use item of table VI to verify compliance with
the requirements of 3.3.3.
4.6.2.4 Starting torque. Use item 1 of table VI to verify compliance
with the requirements of 3.3.4.
4.6.3 Environmental tests.
4.6.3.1 Shock.
4.6.3.1.1 Basic design. Use items 4, 5 and 6 of table VI and subject the
assembly to the shock test specified in MIL-STD-81O, method 516.2, procedure I
figure 516.2-2. Apply three half since wave shock pulses in each direction
along the three axes. Peak amplitude shall be 50 5 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 4.6.2.
4.6.3.1.2 High intensity. Use items 4, and 6 of table Vi and subject
the assembly to the shock test specified in MIL-STD-81O, method 516.2,
procedure IV, figure 516.2-2. Apply three half sine wave shock PUIS e S in each
direction along the three axes. Peak amplitude shall be 125.0 12.5 g with a
time duration of 0.6 0.2 msec measured at the 10 percent amplitude points.
At the conclusion of this test, subject the assembly to the performance tests
of 4.6.2.
4.6.3.2 Vibration. Application of Vibration A and Vibration B shall be
as determined by the procurement conditions of 4.5.1 and the first article
conditions of 4.4.
4.5.3.2.1 Vibration A. Use items 5, 6, 7 and 8 of table VI and subject
the assembly to the vibration test specified in MIL-STD-810, method 514.2,
proceure VIII, except that the test level shall be the vibration curve shown
in figure 4 and duration of exposure shall be no: less than 80 minutes per
axis. At the conclusion of this test, subject the assembly to the performance
tests of 4.6.2.
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