MIL-DTL-87255A(USAF)
FIGURE 4. Anti-g valve outlet pressure vs Gz.
3.5.4 Anti-chatter.
3.5.5
Outlet pressure response
3.5.5.1 Response time.
When the acceleration force is being applied by a centrifuge or an aircraft, the outlet pressure
shall be in accordance with table I (see figure 4) within 2 seconds after the application of the
force. When the acceleration force is being decreased, the pressure shall be in accordance
with table I (see figure 4) within 5 seconds after decreasing the force. Additionally, the outlet
pressure shall change in a smooth continuous manner without oscillations or step responses.
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