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|  MIL-G-81065A(OS)
Table II
Vibration Schedule
Double
Acceleration
Unit
Frequency
Amplitude
cps
in. minimum
(g) minimum
Condition
0.75
Energized
5-6
1.3
6-16
0.1
16-24
3.0
24-40
0.036
40-74
10.0
74-500
3.4.2 Shock
3.4.2.1 The gyro-pendulum shall be capable of withstanding shock as
specified in Table III.
Table III
Shock Schedule
Unit
Minimum Duration
Acceleration
Peak Magnitude
Direction
Condition
(g's)
I
Nonoperating
8.0
Any
60
Ready, non-
operating
Fwd
20.0
45
Ready
0.5
Any
85
0.5
Aft
300
3.4.2.2 Shock; transportation, storage, and handling. The gyro-pendulum,
after being subjected to the test specified in 4.5.2.2.2, shall show no
damage and shall meet all the requirements of Section 3.
3.4.3 Acceleration. The gyro-pendulum shall be capable of withstanding
the accelerations specified in Table IV.
10
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