NSN 5990-00-188-6111

Part Details | ELECTRICAL RESOLVER

5990-00-188-6111 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: A15016, 11RP4, 10243514, 5990-00-188-6111, 00-188-6111, 5990001886111, 001886111

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59MAR 01, 197100-188-611122966 ( RESOLVER, ELECTRICAL )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

Cross Reference | NSN 5990-00-188-6111
Part Number Cage Code Manufacturer
A1501605584AUTODYNE MANUFACTURING CO., INC.
11RP408719DUCOMMUN LABARGE TECHNOLOGIES, INCDBA AMERICAN ELECTRONICS
1024351418876U S ARMY AVIATION AND MISSILECOMMAND
Technical Data | NSN 5990-00-188-6111
Characteristic Specifications
BODY SIZE11
STATOR INPUT VOLTAGE RATING IN VOLTS0.5 MINIMUM AND 26.0 MAXIMUM
STATOR INPUT CURRENT RATING6.5 MILLIAMPERES MAXIMUM
STATOR INPUT ELECTRICAL POWER RATING20.0 MILLIWATTS MAXIMUM
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS440.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS2080.00 NOMINAL
ZSO RESISTANCE IN OHMS385.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS1960.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS530.00 NOMINAL
STATOR DC RESISTANCE IN OHMS305.00 NOMINAL
TRANSFORMATION RATIO0.975 ROTOR TO STATOR NOMINAL
COMPENSATION METHOD WINDING COMPENSATED
COMPENSATOR DC RESISTANCE IN OHMS530.00 NOMINAL
COMPENSATOR TRANSFORMATION RATIO IN PERCENT0.980 ROTOR TO COMPENSATOR NOMINAL
PHASE SHIFT ANGLE IN DEG8.500 INPUT TO OUTPUT NOMINAL
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT1.00 INPUT
INTERAXIS ERROR ANGULAR RANGE IN MINUTESM5.0/P5.0
OUTPUT VOLTAGE FUNCTIONAL ERROR RANGE IN PERCENTM0.1/P0.1
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS8.0 CENTIMETER-GRAMS NOMINAL
BODY STYLE STANDARD ROUND C
SHOULDER DIAMETER0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM
PILOT DIAMETER0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM
OVERALL LENGTH2.3080 INCHES MAXIMUM
FLANGE DIAMETER1.0620 INCHES NOMINAL
FLANGE THICKNESS0.0930 INCHES NOMINAL
UNDERCUT DIAMETER0.9750 INCHES NOMINAL
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0620 INCHES NOMINAL
SHOULDER LENGTH0.0620 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.9700 INCHES MAXIMUM
ALIGNMENT HOLE DEPTH0.1250 INCHES NOMINAL
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.8120 INCHES NOMINAL
ALIGNMENT HOLE QUANTITY4
TERMINAL TYPE AND QUANTITY12 SCREW
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, CORROSION RESISTING
ZCO RESISTANCE IN OHMS600.00 NOMINAL
PLUS J ZCO REACTANCE IN OHMS2000.00 NOMINAL
END ITEM IDENTIFICATIONGUIDED MISSILE, INTERCEPT