MIL-S-85565(AS)
e.
Low temperature (operating) (see 4.8.5).
f.
Humidity (see 4.8.7).
3.2.4.2 Duty cycle and readiness time. The servo shall contain suf-
ficient energy to perform the flight profile shown in Table I with both
axes operating while restrained with 84 ±2 inch-pound per degree (in-lb/
deg) coaxial loading. One axis shall lag the run time shown in Table I by
0.5 ±1 second. The-servo shall accept an external electr ical signal of 2.8
amps to the electro-initiator and provide a torque output of not less than
900 in-lb within 0.8 second. The electro-initiator shall function within
50 ms.
TABLE I.
Duty cycle (leading axis).
1/ Actuation at 0.0 second.
2/ The torque specified shall be met during any portion of the
step input.
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