BODY SIZE | 10 |
STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
STATOR INPUT CURRENT RATING | 42.0 MILLIAMPERES NOMINAL |
STATOR INPUT ELECTRICAL POWER RATING | 103.0 MILLIWATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ZRO RESISTANCE IN OHMS | 85.40 NOMINAL |
PLUS J ZRO REACTANCE IN OHMS | 281.00 NOMINAL |
ZSO RESISTANCE IN OHMS | 77.60 NOMINAL |
PLUS J ZSO REACTANCE IN OHMS | 363.00 NOMINAL |
ZRS RESISTANCE IN OHMS | 84.30 NOMINAL |
PLUS J ZRS REACTANCE IN OHMS | 31.10 NOMINAL |
ROTOR DC RESISTANCE IN OHMS | 75.50 NOMINAL |
STATOR DC RESISTANCE IN OHMS | 41.00 NOMINAL |
TRANSFORMATION RATIO | 1.041 STATOR TO ROTOR NOMINAL |
PHASE SHIFT ANGLE IN DEG | 10.800 OUTPUT TO INPUT NOMINAL |
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | -7.0 TO 7.0 |
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 6.0 CENTIMETER-GRAMS NOMINAL |
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS NOMINAL |
BODY STYLE | STANDARD ROUND C |
SHOULDER DIAMETER | 1.0000 INCHES NOMINAL |
PILOT DIAMETER | 0.5000 INCHES NOMINAL |
OVERALL LENGTH | 1.6280 INCHES MAXIMUM |
FLANGE DIAMETER | 0.9370 INCHES NOMINAL |
FLANGE THICKNESS | 0.1250 INCHES NOMINAL |
UNDERCUT DIAMETER | 0.8123 INCHES NOMINAL |
UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
PILOT LENGTH | 0.0380 INCHES NOMINAL |
SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2400 INCHES MAXIMUM |
ALIGNMENT HOLE DEPTH | 0.1000 INCHES NOMINAL |
ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.6780 INCHES NOMINAL |
ALIGNMENT HOLE QUANTITY | 3 |
SHAFT TYPE | ROUND, SLOTTED SINGLE SHAFT |
SHAFT DIAMETER | 0.0900 INCHES NOMINAL SINGLE SHAFT |
SHAFT LENGTH | 0.4130 INCHES NOMINAL SINGLE SHAFT |
SHAFT SLOT DEPTH | 0.0300 INCHES NOMINAL SINGLE SHAFT |
SHAFT SLOT WIDTH | 0.0200 INCHES NOMINAL SINGLE SHAFT |
TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
TERMINAL LOCATION | REAR |
BODY MATERIAL | STEEL, CORROSION RESISTING |
SPECIAL FEATURES | RESOLVER IS CRITICAL FOR FIT FORM AND FUNCTION TOLERANCE AND APPLICATION FOR THE AMPLIFIER POWER SUPPLY FOR THE E-3 AIRCRAFT |
CRITICALITY CODE JUSTIFICATION | FEAT |
FRAGILITY FACTOR | MODERATELY RUGGED |