NSN 5990-00-936-3947

Part Details | ELECTRICAL RESOLVER

5990-00-936-3947 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: 13846501, 138465-01, CSH8LE3L148, 5990-00-936-3947, 00-936-3947, 5990009363947, 009363947

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59MAR 03, 196700-936-394722966 ( RESOLVER, ELECTRICAL )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND A

Cross Reference | NSN 5990-00-936-3947
Part Number Cage Code Manufacturer
138465-0135351GE AVIATION SYSTEMS LLC
CSH8LE3L14899932MOOG INC.DBA MOOG COMPONENTS GROUP
Technical Data | NSN 5990-00-936-3947
Characteristic Specifications
BODY SIZE8
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
ROTOR INPUT CURRENT RATING15.0 MILLIAMPERES MAXIMUM
ROTOR INPUT ELECTRICAL POWER RATING110.0 MILLIWATTS MAXIMUM
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS916.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS2430.00 NOMINAL
ZSO RESISTANCE IN OHMS206.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS737.00 NOMINAL
ZRS RESISTANCE IN OHMS1210.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS258.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS725.00 NOMINAL
STATOR DC RESISTANCE IN OHMS160.00 NOMINAL
TRANSFORMATION RATIO0.477 STATOR TO ROTOR NOMINAL
TRANSFORMATION RATIO EQUALITY IN PERCENT3.5 NOMINAL
PHASE SHIFT ANGLE IN DEG17.000 INPUT TO OUTPUT MINIMUM AND 20.000 INPUT TO OUTPUT MAXIMUM
MAXIMUM TEMP RISE6.0 DEG CELSIUS
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT30.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM7.0/P7.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS9.0 CENTIMETER-GRAMS MAXIMUM
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS3.0 CENTIMETER-GRAMS MAXIMUM
BODY STYLE STANDARD ROUND A
PILOT DIAMETER0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM
OVERALL LENGTH1.7050 INCHES MINIMUM AND 1.7450 INCHES MAXIMUM
FLANGE DIAMETER0.7490 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM
FLANGE THICKNESS0.0620 INCHES NOMINAL
UNDERCUT DIAMETER0.6910 INCHES MAXIMUM
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0430 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2450 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY7 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, CORROSION RESISTING