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|  MIL-R-48595A(AR)
4.6.2.8 Light dimming control. Use item 1 of table IX to determine
compliance with 3.3.8.
4.6.2.9 LIGHT switch. Use item 1 of table IX to determine compliance
with 3.3.9.
4.6.2.10 Peak output power. Use item I of table IX to determine
compliance with 3.3.100
4.6.2.11 Input voltage variation. Use item 1, 6 and 7 of table IX to
determine compliance with 3.3.11.
Use item 1 of table IX to determine compliance
4.6.2.12 Power drain.
with 3.3.12.
Use item 1 of table IX to determine
4.6.2.13 Primary power transient.
compliance with 3.3.13.
Use item 1 of table IX to determine
4.6.2.14 Transmitter test.
compliance with 3.3.14.
Use item 1 of table IX to determine compliance
4.6.2.15 Built-in test.
with 3.3.15.
4.6.2.16 Remote controlled operations. Use item 1 of table IX to
determine compliance with 3.3.16.
Use item 1 of table IX to determine compliance
4.6.2.17 Sight system.
with 3.3.17.
Use item 1 of table IX to determine
4.6.2.18 Optical operability.
compliance with 3.3.18.
4.6.2.19 Sight system and laser beam alignment. Use item 1 of table IX
to determine compliance with 3.3.19.
4.6.3 Environmental tests.
4.6.3.1 Shock.
4.6.3.1.1 Basic design . Use item 2 of table IX and subject the
rangefinder to the shock test specified in MIL-STD-810, method 516.2,
procedure I, figure 516.2-. Apply three half sine wave shock pulsein each
direction along the three axes. Peak amiplitude 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 rangefinder to the performance tests of
table VI.
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