NSN 5990-00-010-8176

Part Details | ELECTRICAL RESOLVER

5990-00-010-8176 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: CM41034108, CM41034108, HWC8TRVF05F215, HWC-8T-RVF-05/F215, HVC8TRVF2F026, HVC-8T-RVF-2/F026, HVC8RVF2L555, HVC-8-RVF-2/L555, 5317071, 531707-1, 5990-00-010-8176, 00-010-8176, 5990000108176, 000108176

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59MAY 08, 196800-010-817622966 ( RESOLVER, ELECTRICAL )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND A

2 ROTOR, 2 STATOR

Cross Reference | NSN 5990-00-010-8176
Part Number Cage Code Manufacturer
CM4103410888818KEARFOTT CORPORATIONDBA KEARFOTT
CM4103410805088KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS
HWC-8T-RVF-05/F21599932MOOG INC.DBA MOOG COMPONENTS GROUP
HVC-8T-RVF-2/F02699932MOOG INC.DBA MOOG COMPONENTS GROUP
HVC-8-RVF-2/L55599932MOOG INC.DBA MOOG COMPONENTS GROUP
531707-196214RAYTHEON COMPANYDBA RAYTHEON
Technical Data | NSN 5990-00-010-8176
Characteristic Specifications
BODY SIZE8
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
ROTOR INPUT CURRENT RATING45.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING280.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS137.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS558.00 NOMINAL
ZSO RESISTANCE IN OHMS30.20 NOMINAL
PLUS J ZSO REACTANCE IN OHMS137.00 NOMINAL
ZRS RESISTANCE IN OHMS193.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS70.00 NOMINAL
ZSS IMPEDANCE MAGNITUDE IN OHMS50.00 NOMINAL
ZSS IMPEDANCE ANGLE IN DEG21.60 NOMINAL
ROTOR DC RESISTANCE IN OHMS130.00 NOMINAL
STATOR DC RESISTANCE IN OHMS22.70 NOMINAL
TRANSFORMATION RATIO0.436 STATOR TO ROTOR NOMINAL
PHASE SHIFT ANGLE IN DEG11.000 INPUT TO OUTPUT NOMINAL
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT20.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM8.0/P8.0
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 LENGTH1.9050 INCHES MAXIMUM
FLANGE DIAMETER0.7500 INCHES MAXIMUM
FLANGE THICKNESS0.0620 INCHES NOMINAL
UNDERCUT DIAMETER0.6910 INCHES MAXIMUM
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0400 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.4200 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY6 WIRE LEAD
TERMINAL LOCATION SIDE
BODY MATERIAL STEEL, STAINLESS
SHAFT MAXIMUM RADIAL PLAY0.0008 INCHES
SHAFT RADIAL PLAY TEST POINT0.125 INCHES MAXIMUM
SHAFT RADIAL PLAY DETERMINING WEIGHT4.0 OUNCES
SHAFT END PLAY0.0005 INCHES MINIMUM AND 0.0015 INCHES MAXIMUM
SHAFT END PLAY DETERMINING WEIGHT8.0 OUNCES
SHAFT MAXIMUM RUNOUT0.0010 INCHES
SCHEMATIC DIAGRAM DESIGNATOR4 2 ROTOR, 2 STATOR
TERMINAL DESIGNATOR AND SCHEMATIC POSITION CONNECTION R1 POSITION A AND CONNECTION R2 POSITION B AND CONNECTION S1 POSITION H AND CONNECTION S2 POSITION F AND CONNECTION S3 POSITION J AND CONNECTION S4 POSITION E
FRAGILITY FACTOR MODERATELY RUGGED
END ITEM IDENTIFICATION5841-00-403-7520