NATO Stock Number
5990-00-922-2449
Sold in multiples of
1 EA
DEMIL
NO
Body Material
Any acceptable
Body Style
Standard round b
Shoulder Diameter
Between 0.9995 inches and 1.0000 inches
Pilot Diameter
Between 0.6245 inches and 0.6250 inches
Overall Length
2.3560 inches
Flange Diameter
Between 1.0570 inches and 1.0620 inches
Flange Thickness
0.0930 inches
Undercut Width
0.0500 inches
Shaft Diameter
0.1867 inches single shaft and 0.1872 inches single shaft
Shaft Length
0.5000 inches single shaft
Fragility Factor
Moderately rugged
Maximum Tempurature Rise
20.0 degrees celsius
Body Size
11
Rotor Input Voltage Rating In Volts
Between 114.0 and 116.0
Frequency In Hertz
Between 396.0 and 404.0
Rotor Input Current Rating
31.0 milliamperes
Rotor Input Electrical Power Rating
490.0 milliwatts
Zro Impedance Magnitude In Ohms
Between 3720.00 and 4700.00
Zro Impedance Angle In Deg
Between 80.00 and 84.00
Zss Impedance Magnitude In Ohms
Between 410.00 and 500.00
Zss Impedance Angle In Deg
Between 17.00 and 26.00
Phase Shift Angle In Deg
Between 3.000 input to output and 6.000 input to output
Maximum Fundamental Null Voltage In Millivolts Per Volt
45.00 output
Maximum Total Null Voltage Output In Millivolts Per Volt
75.00
Actuator Friction Torque At Plus 25 Deg Celsius
0.07 inch-ounces
Alignment Hole Quantity
4
Pilot Length
0.0620 inches
Shoulder Length
0.0620 inches
Mounting Surface To Terminal End Distance
1.7320 inches
Terminal Location
Rear
Shaft Type
Round single shaft
Alignment Hole Depth
0.1250 inches
Transformation Ratio
0.783 stator to rotor
Alignment Hole Bolt Circle Diameter
Between 0.8090 inches and 0.8150 inches
Test Data Document
18876-10181799 drawing (this is the basic governing drawing, such as a contractor drawing, original equipment manufacturer drawing, etc.; excludes any specification, standard or other document that may be referenced in a basic governing drawing)
Terminal Type And Quantity
5 screw
