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| ![]() MIL-V-82440(OS)
TABLE VII
ACCELERATION SCHEDULE
Acceleration Direction
`s 10%)
( See Figure 1 )
Magnitude
Time
Longitudinal axis, Fwd
25
1 minute
Longitudinal axis, Aft
35
1 minute
4.4.4.4
Shock, ready condition. The valve, in the ready condition,
shall be attached to a shock test machine (see Figure..l). Shock
magnitudes and durations shall be measured by an accelerometer mounted
on the mounting fixture. Tests on the valve shall be performed in
accordance with Table VIII in the sequence shown.
TABLE VIII
SHOCK TEST SCHEDULE
Peak
Direction Of Number
Magnitude
Test
Impact
Deceleration Of
Duration
(g 's 10%)
Sequence
(ms)
Axis
Force
Impacts
1
to 1.5 Longitudinal
300
0.5
Aft
3
2
0.5
to 1.5 Transverse A
Optional
85
3
to 1.5 Transverse B
3
85
0.5
Optional
3
4
18.0
to 20.0 Longitudinal
45
Fwd
3
60
5
to 10.0 Longitudinal
8.0
Aft
3
6
to 10.0 Longitudinal
60
8.0
Fwd
3
60
7
Optional
to 10.0 Transverse A
8.0
3
3
8
60
Optional
8.0
to 10.0 Transverse B
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