NSN 5990-00-104-1617

Part Details | ELECTRICAL RESOLVER

5990-00-104-1617 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: BQC11BZS01B226, 529686, 5990-00-104-1617, 00-104-1617, 5990001041617, 001041617

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JUN 14, 196800-104-161722966 ( RESOLVER, ELECTRICAL )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND B

Cross Reference | NSN 5990-00-104-1617
Part Number Cage Code Manufacturer
BQC11BZS01B22699932MOOG INC.DBA MOOG COMPONENTS GROUP
52968636378RAYTHEON TECHNICAL SERVICES COMPANY
Technical Data | NSN 5990-00-104-1617
Characteristic Specifications
BODY SIZE11
STATOR INPUT VOLTAGE RATING IN VOLTS22.0 NOMINAL
STATOR INPUT CURRENT RATING4.5 MILLIAMPERES MINIMUM AND 10.0 MILLIAMPERES MAXIMUM
STATOR INPUT ELECTRICAL POWER RATING6.7 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS500.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS2325.00 NOMINAL
ZSO RESISTANCE IN OHMS360.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS2200.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS425.00 NOMINAL
STATOR DC RESISTANCE IN OHMS280.00 NOMINAL
TRANSFORMATION RATIO0.980 ROTOR TO STATOR NOMINAL
TRANSFORMATION RATIO EQUALITY IN PERCENT0.2 NOMINAL
COMPENSATION METHOD RESISTOR COMPENSATED
COMPENSATOR DC RESISTANCE IN OHMS430.00 NOMINAL
COMPENSATOR TRANSFORMATION RATIO IN PERCENT1.007 ROTOR TO COMPENSATOR NOMINAL
PHASE SHIFT ANGLE IN DEG7.000 INPUT TO OUTPUT NOMINAL
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT8.00 OUTPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT10.00
INTERAXIS ERROR ANGULAR RANGE IN MINUTESM3.0/P3.0
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM3.5/P3.5
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS16.0 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS4.0 CENTIMETER-GRAMS NOMINAL
BODY STYLE STANDARD ROUND B
SHOULDER DIAMETER0.9997 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM
PILOT DIAMETER0.6247 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM
OVERALL LENGTH2.3580 INCHES MINIMUM AND 2.3730 INCHES MAXIMUM
FLANGE DIAMETER1.0610 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM
FLANGE THICKNESS0.0930 INCHES NOMINAL
UNDERCUT WIDTH0.0500 INCHES NOMINAL
PILOT LENGTH0.0620 INCHES NOMINAL
SHOULDER LENGTH0.0620 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.8200 INCHES MINIMUM AND 1.8350 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, STAINLESS
ZCO RESISTANCE IN OHMS480.00 NOMINAL
PLUS J ZCO REACTANCE IN OHMS2200.00 NOMINAL