NSN 5990-00-847-1164

Part Details | ELECTRICAL RESOLVER

5990-00-847-1164 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: AY52346A1, AY523-46A1, NA714056PC5, 2003167PC5, 5990-00-847-1164, 00-847-1164, 5990008471164, 008471164

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 01, 196200-847-116422966 ( RESOLVER, ELECTRICAL )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

Cross Reference | NSN 5990-00-847-1164
Part Number Cage Code Manufacturer
AY523-46A155972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
NA714056PC556232LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN
2003167PC510001NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT
Technical Data | NSN 5990-00-847-1164
Characteristic Specifications
BODY SIZE10
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
ROTOR INPUT CURRENT RATING55.0 MILLIAMPERES MAXIMUM
ROTOR INPUT ELECTRICAL POWER RATING600.0 MILLIWATTS MAXIMUM
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 OHMS42.00 NOMINAL
TRANSFORMATION RATIO0.454 ROTOR TO STATOR NOMINAL
TRANSFORMATION RATIO EQUALITY IN PERCENT3.0 NOMINAL
PHASE SHIFT ANGLE IN DEG17.000 INPUT TO OUTPUT MAXIMUM
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT60.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM18.0/P18.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS25.00 CENTIMETER-GRAMS MAXIMUM
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS7.00 CENTIMETER-GRAMS MAXIMUM
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 NOMINAL
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 LENGTH0.0630 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2410 INCHES NOMINAL
ALIGNMENT HOLE DEPTH0.0630 INCHES MAXIMUM
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.6780 INCHES NOMINAL
ALIGNMENT HOLE QUANTITY4
TERMINAL TYPE AND QUANTITY7 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, STAINLESS