ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | -10.0 TO 10.0 |
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 6.00 CENTIMETER-GRAMS MAXIMUM |
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.00 CENTIMETER-GRAMS MAXIMUM |
BODY MATERIAL | ALUMINUM |
BODY SIZE | 15 |
BODY STYLE | STANDARD ROUND C |
FLANGE DIAMETER | 1.4360 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM |
FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
FRAGILITY FACTOR | MODERATELY RUGGED |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
OVERALL LENGTH | 2.1620 INCHES NOMINAL |
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 25.00 OUTPUT |
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6220 INCHES NOMINAL |
SHOULDER LENGTH | 0.1320 INCHES NOMINAL |
PHASE SHIFT ANGLE IN DEG | 4.000 INPUT TO OUTPUT NOMINAL |
PILOT LENGTH | 0.0400 INCHES NOMINAL |
PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
PLUS J ZRO REACTANCE IN OHMS | 3000.00 NOMINAL |
PLUS J ZRS REACTANCE IN OHMS | 290.00 NOMINAL |
PLUS J ZSO REACTANCE IN OHMS | 26.40 NOMINAL |
ROTOR INPUT CURRENT RATING | 60.0 MILLIAMPERES MAXIMUM |
ROTOR INPUT ELECTRICAL POWER RATING | 800.0 MILLIWATTS MAXIMUM |
ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
SHAFT DIAMETER | 0.1195 INCHES MINIMUM AND 0.1200 INCHES MAXIMUM SINGLE SHAFT |
SHAFT SLOT DEPTH | 0.0220 INCHES MINIMUM AND 0.0320 INCHES MAXIMUM SINGLE SHAFT |
SHAFT SLOT WIDTH | 0.0220 INCHES MINIMUM AND 0.0320 INCHES MAXIMUM SINGLE SHAFT |
SHAFT LENGTH | 0.5400 INCHES NOMINAL SINGLE SHAFT |
SHAFT TYPE | ROUND, SLOTTED SINGLE SHAFT |
SHOULDER DIAMETER | 1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM |
UNDERCUT DIAMETER | 1.3090 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM |
UNDERCUT WIDTH | 0.0780 INCHES NOMINAL |
ZRO RESISTANCE IN OHMS | 520.00 NOMINAL |
ZRS RESISTANCE IN OHMS | 444.00 NOMINAL |
ZSO RESISTANCE IN OHMS | 5.70 NOMINAL |
TERMINAL LOCATION | REAR |
TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
TORQUE GRADIENT PER ANGULAR DEG | 3000.0 MILLIMETER-MILLIGRAMS NOMINAL |
TRANSFORMATION RATIO | 0.103 ROTOR TO STATOR NOMINAL |