NSN 5990-00-007-7833

Part Details | ELECTRICAL RESOLVER

5990-00-007-7833 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: AY523G47A2, 5990-00-007-7833, 00-007-7833, 5990000077833, 000077833

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JUL 12, 197200-007-783322966 ( RESOLVER, ELECTRICAL )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

RESOLVER,ELECTRICAL | 5990-00-007-7833, 000077833

2 ROTOR, 2 STATOR

RESOLVER,ELECTRICAL | 5990-00-007-7833, 000077833
Cross Reference | NSN 5990-00-007-7833
Part Number Cage Code Manufacturer
AY523G47A255972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
Technical Data | NSN 5990-00-007-7833
Characteristic Specifications
BODY SIZE10
STATOR INPUT VOLTAGE RATING IN VOLTS5.0 NOMINAL
STATOR INPUT CURRENT RATING2.8 MILLIAMPERES NOMINAL
STATOR INPUT ELECTRICAL POWER RATING3.6 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZSO RESISTANCE IN OHMS457.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS1727.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS364.00 NOMINAL
STATOR DC RESISTANCE IN OHMS304.00 NOMINAL
TRANSFORMATION RATIO0.767 STATOR TO ROTOR NOMINAL
PHASE SHIFT ANGLE IN DEG10.000 INPUT TO OUTPUT NOMINAL
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT40.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM30.0/P30.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS30.00 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS10.00 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 NOMINAL
FLANGE DIAMETER0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM
FLANGE THICKNESS0.0625 INCHES NOMINAL
UNDERCUT DIAMETER0.8350 INCHES MINIMUM AND 0.8400 INCHES MAXIMUM
UNDERCUT WIDTH0.0625 INCHES NOMINAL
PILOT LENGTH0.0380 INCHES NOMINAL
SHOULDER LENGTH0.0625 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2410 INCHES MAXIMUM
ALIGNMENT HOLE DEPTH0.0781 INCHES NOMINAL
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.6750 INCHES MINIMUM AND 0.6810 INCHES MAXIMUM
ALIGNMENT HOLE QUANTITY3
TERMINAL TYPE AND QUANTITY7 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, STAINLESS
SHAFT MAXIMUM RADIAL PLAY0.0008 INCHES
SHAFT RADIAL PLAY TEST POINT0.125 INCHES MAXIMUM
SHAFT RADIAL PLAY DETERMINING WEIGHT1.4 OUNCES
SHAFT END PLAY0.0001 INCHES MINIMUM AND 0.0005 INCHES MAXIMUM
SHAFT END PLAY DETERMINING WEIGHT3.0 OUNCES
SHAFT MAXIMUM RUNOUT0.0010 INCHES
SCHEMATIC DIAGRAM DESIGNATOR3 2 ROTOR, 2 STATOR
TERMINAL DESIGNATOR AND SCHEMATIC POSITION CONNECTION R1 POSITION A AND CONNECTION R2 POSITION B AND CONNECTION R3 POSITION C AND CONNECTION S1 POSITION H AND CONNECTION S2 POSITION E AND CONNECTION S3 POSITION J AND CONNECTION S4 POSITION F
FRAGILITY FACTOR MODERATELY RUGGED