NSN 5990-00-838-0696

Part Details | ELECTRICAL RESOLVER

5990-00-838-0696 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: 101231REVA, 10123-1REVA, 101231, 10123-1, CR40931018, CR40939007, TSH11G08A050, 5990-00-838-0696, 00-838-0696, 5990008380696, 008380696

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59DEC 09, 196600-838-069622966 ( RESOLVER, ELECTRICAL )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

2 ROTOR, 2 STATOR

Cross Reference | NSN 5990-00-838-0696
Part Number Cage Code Manufacturer
10123-1REVA10138ASTRONAUTICS CORPORATION OF AMERICA
10123-110138ASTRONAUTICS CORPORATION OF AMERICA
CR4093101888818KEARFOTT CORPORATIONDBA KEARFOTT
CR4093900705088KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS
TSH11G08A05099932MOOG INC.DBA MOOG COMPONENTS GROUP
Technical Data | NSN 5990-00-838-0696
Characteristic Specifications
BODY SIZE11
STATOR INPUT VOLTAGE RATING IN VOLTS22.0 NOMINAL
STATOR INPUT CURRENT RATING17.8 MILLIAMPERES NOMINAL
STATOR INPUT ELECTRICAL POWER RATING88.0 MILLIWATTS NOMINAL
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
ROTOR INPUT CURRENT RATING17.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING90.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS310.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS1500.00 NOMINAL
ZSO RESISTANCE IN OHMS280.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS1200.00 NOMINAL
ZRS RESISTANCE IN OHMS53.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS23.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS190.00 NOMINAL
STATOR DC RESISTANCE IN OHMS170.00 NOMINAL
PHASE SHIFT ANGLE IN DEG7.000 INPUT TO OUTPUT NOMINAL
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT26.00 INPUT
INTERAXIS ERROR ANGULAR RANGE IN MINUTESM7.0/P7.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS16.00 CENTIMETER-GRAMS MAXIMUM
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS4.00 CENTIMETER-GRAMS MAXIMUM
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 LENGTH2.0840 INCHES NOMINAL
FLANGE DIAMETER1.0570 INCHES MINIMUM AND 1.0650 INCHES MAXIMUM
FLANGE THICKNESS0.0930 INCHES NOMINAL
UNDERCUT DIAMETER0.9750 INCHES NOMINAL
UNDERCUT WIDTH0.0500 INCHES NOMINAL
PILOT LENGTH0.0620 INCHES NOMINAL
SHOULDER LENGTH0.0620 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.6440 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY7 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, STAINLESS
SHAFT MAXIMUM RADIAL PLAY0.0008 INCHES
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 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 F AND CONNECTION S3 POSITION J AND CONNECTION S3 POSITION E
FRAGILITY FACTOR MODERATELY RUGGED