NSN 5990-00-132-0187

Part Details | ELECTRICAL RESOLVER

5990-00-132-0187 An item consisting of a rotor and a stator inductively coupled. It usually has two rotor windings displaced from each other by 90 degrees and two stator windings similarly displaced. The output voltage(s) is a trigonometric function of the input voltage(s) and the angular displacement of the rotor with respect to the stator. See also SYNCHRO (as modified) and GONIOMETER, ELECTRICAL. Excludes TRANSOLVER, ELECTRICAL and potentiometer sine/cosine electrical resolvers.

Alternate Parts: AY52325A1, AY523-25A1, 5990-00-132-0187, 00-132-0187, 5990001320187, 001320187

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59DEC 20, 196800-132-018722966 ( RESOLVER, ELECTRICAL )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

Cross Reference | NSN 5990-00-132-0187
Part Number Cage Code Manufacturer
AY523-25A155972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
Technical Data | NSN 5990-00-132-0187
Characteristic Specifications
BODY SIZE10
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
ROTOR INPUT CURRENT RATING40.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING350.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS268.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS620.00 NOMINAL
ZSO RESISTANCE IN OHMS65.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS188.00 NOMINAL
ZRS RESISTANCE IN OHMS342.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS118.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS200.00 NOMINAL
STATOR DC RESISTANCE IN OHMS41.00 NOMINAL
PHASE SHIFT ANGLE IN DEG17.0000 INPUT TO OUTPUT NOMINAL
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT75.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM18.0/P18.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS0.5 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS0.3 CENTIMETER-GRAMS NOMINAL
BODY STYLE STANDARD ROUND C
SHOULDER DIAMETER0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM
PILOT DIAMETER0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM
OVERALL LENGTH1.6540 INCHES MAXIMUM
FLANGE DIAMETER0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM
FLANGE THICKNESS0.0620 INCHES NOMINAL
UNDERCUT DIAMETER0.8350 INCHES MINIMUM AND 0.8400 INCHES MAXIMUM
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0380 INCHES NOMINAL
SHOULDER LENGTH0.0620 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2410 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY7 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, CORROSION RESISTING