NSN 5990-00-819-5617

Part Details | ELECTRICAL RESOLVER

5990-00-819-5617 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: 4558511, 455851-1, 4558511, 455851-1, 5990-00-819-5617, 00-819-5617, 5990008195617, 008195617

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 01, 196200-819-561722966 ( RESOLVER, ELECTRICAL )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND A

2 ROTOR, 1 STATOR

Cross Reference | NSN 5990-00-819-5617
Part Number Cage Code Manufacturer
455851-199932MOOG INC.DBA MOOG COMPONENTS GROUP
455851-196214RAYTHEON COMPANYDBA RAYTHEON
Technical Data | NSN 5990-00-819-5617
Characteristic Specifications
BODY SIZE8
STATOR INPUT VOLTAGE RATING IN VOLTS15.0 NOMINAL
STATOR INPUT CURRENT RATING18.2 MILLIAMPERES NOMINAL
STATOR INPUT ELECTRICAL POWER RATING58.0 MILLIWATTS NOMINAL
ROTOR INPUT VOLTAGE RATING IN VOLTS15.0 NOMINAL
ROTOR INPUT CURRENT RATING22.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING110.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS230.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS640.00 NOMINAL
ZSO RESISTANCE IN OHMS176.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS806.00 NOMINAL
ZRS RESISTANCE IN OHMS330.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS71.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS220.00 NOMINAL
STATOR DC RESISTANCE IN OHMS158.00 NOMINAL
TRANSFORMATION RATIO EQUALITY IN PERCENT0.5 MAXIMUM
PHASE SHIFT ANGLE IN DEG11.000 OUTPUT TO INPUT NOMINAL
MAXIMUM TEMP RISE20.0 DEG CELSIUS
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT22.00 INPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT30.00
INTERAXIS ERROR ANGULAR RANGE IN MINUTESM5.0/P5.0
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 DIAMETER0.5000 INCHES MAXIMUM
OVERALL LENGTH1.7620 INCHES MAXIMUM
FLANGE DIAMETER0.7500 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 DISTANCE1.4160 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY8 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL ALUMINUM
SHAFT MAXIMUM RADIAL PLAY0.0008 INCHES
SHAFT RADIAL PLAY TEST POINT0.125 INCHES MAXIMUM
SHAFT RADIAL PLAY DETERMINING WEIGHT4.0 OUNCES
SHAFT END PLAY0.0015 INCHES MAXIMUM
SHAFT END PLAY DETERMINING WEIGHT8.0 OUNCES
SHAFT MAXIMUM RUNOUT0.0010 INCHES
SCHEMATIC DIAGRAM DESIGNATOR2 2 ROTOR, 1 STATOR
TERMINAL DESIGNATOR AND SCHEMATIC POSITION CONNECTION R1 POSITION B AND CONNECTION R2 POSITION C AND CONNECTION R3 POSITION A AND CONNECTION R4 POSITION D AND CONNECTION S1 POSITION H AND CONNECTION S2 POSITION E AND CONNECTION S3 POSITION G AND CONNECTION S3 POSITION F
FRAGILITY FACTOR MODERATELY RUGGED