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3.3.4 Reset. With the digital type-B signal specified in table I applied
to P1-3 and P1-2 as shown in figure 4, the output signal at P1-29 shall be as
shown in figure 4. (See 4.6.2.4)
3.3.5 Malfunction 4 logic. With the digital type-A signals specified in
table I applied to pins as listed in table II, the Malfunction 4 signal at
P1-19 shall be as listed in table II. (See 4.6.2.5)
3.3.6 +200 Volt malfunction. With the logical zero digital type-A signal
specified in table I momentarily applied to P1-13, the voltage at P1-19 shall
be 4.2-1 Vdc. With the +220 Vdc power source of table I reduced to +145 5
Vdc, the voltage at P1-19 shall be +0.2 0.2 Vdc. (See 4.6.2.6)
3.3.7 Malfunction 2 logic. With the digital type-B signals of table I
applied to pins as listed in table III, the output at P1-17 shall be as listed
in table III. (See 4.6.2.7)
3.3.8 +15V interlock and range light signals. with the digital type-A
signals specified in table I applied to P1-34, the voltages at PI-26 and Pi-27
shall be as listed in table IV. (See 4.6.2.8)
3.3.9 Minimum range inhibit. With the digital type-A signal of table I
applied to P1-6 as shown in figure 5, the output signal at P1-4 shall be as
shown in figure 5. {See 4.6.2.9)
3.3.10 Range signal. With the logical one digital type-A signal of table
I applied to P1-20, the output at P1-30 shall be +0.2 0.2 Vdc. With the
logical zero digital type-A signal of table I applied to P1-20, the output at
P1-30 shall be +4.2 1.O Vdc. (See 4.6.2.10)
3.3.11 Alarm signal. With the logical one digital type-A signal of table
I applied to Pi-26, the output at P1-24 shall be 0.3 0.3 Vdc. With the
logical zero digital type-A signal of table I applied to P1-26, the output at
P1-24 shall be +15.0 1.0 Vdc. (See 4.6.2.11)
3.4 Environmental.
3.4.1 Shock. The assembly shall be capable of operating as specified
herein after exposure under the conditions of 3.1.3 to three half sine wave
shock pulses of 40 4 gravity unit (g) for a duration of 18 3 milliseconds
(rnsec) applied in each direction along three mutually perpendicular axes. In
addition, the assembly shall be capable of withstanding three half sine wave
shock pulses of 100.0 10.0 g for a duration of 1.5 0.2 msec applied in each
direction along three mutually perpendicular axes. (See 4.6.3.1)
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