MIL-DTL-55041/10B
REQUIREMENTS:
Dimensions and configuration: See figure 1.
Exterior surface: Black finish in accordance with MIL-DTL-14072.
Weight: 2.5 pounds (1.13 kg), maximum.
Operation: 1P2T latching, break before make.
Rotor operation: See figure 1, note 4.
Connector: The power connector shall mate with connector MS3116E10-6S.
Drive assembly operation: See figure 1, note 6.
Drive assembly operating voltage: 21 V dc to 29 V dc.
Drive assembly starting current: 4 amperes, maximum, at 27 V dc.
RF power handling capability: Peak 400 kW, average 400 W.
Temperature altitude: The temperature altitude must be as recommended for class 2 equipment
designed for 21.28 Km (70,000 feet) altitude and continuous sea level operation over the temperature
range of -62°C to +90°C (+95 °C intermittent operation).
Frequency range: 8.6 GHz to 10.3 GHz.
Isolation: 80 dB, minimum.
VSWR: 1.1:1, maximum.
Insertion loss: 0.10 dB, maximum.
Switching time (see figure 2):
1 second, maximum, 21 V dc at 20C 10C;
2 seconds, maximum, 21 V dc at -54C 5C.
Pressure: With 30 lbf/in2 (gage) applied, the pressure drop shall not exceed 5 lbf/in2 (gage) in 1 hour.
Pressure equilibrium: 1 lbf/in2, tested as follows:
a. Seal one active (open) waveguide port by means of an O-ring and flat plate and attach a
compressed air (15 lbf/in2 (gage)) input to the other active (open) waveguide port.
b. Adjust flow rate of compressed air to 100 cubic inches per minute.
c.
Measure the pressure differential between the air input port to which the compressed air is
attached and the inactive (closed) waveguide port. The pressure differential shall not exceed the
value specified.
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