NSN 5990-00-145-1187

Part Details | ELECTRICAL RESOLVER

5990-00-145-1187 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: MILR14346, 23R6N6, F7676358, 5990-00-145-1187, 00-145-1187, 5990001451187, 001451187

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59MAY 09, 196900-145-118722966 ( RESOLVER, ELECTRICAL )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND D

Cross Reference | NSN 5990-00-145-1187
Part Number Cage Code Manufacturer
MILR1434681349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
23R6N681349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
F767635819200US ARMY ARDEC RDECOM
Technical Data | NSN 5990-00-145-1187
Characteristic Specifications
BODY SIZE23
ROTOR INPUT VOLTAGE RATING IN VOLTS20.0 MINIMUM AND 90.0 MAXIMUM
ROTOR INPUT CURRENT RATING170.0 MILLIAMPERES MAXIMUM
ROTOR INPUT ELECTRICAL POWER RATING8.0 WATTS MAXIMUM
FREQUENCY IN HERTZ60.0 NOMINAL
ROTOR DC RESISTANCE IN OHMS250.00 NOMINAL
STATOR DC RESISTANCE IN OHMS280.00 NOMINAL
TRANSFORMATION RATIO1.000 STATOR TO ROTOR NOMINAL
TRANSFORMATION RATIO EQUALITY IN PERCENT0.5 NOMINAL
PHASE SHIFT ANGLE IN DEG28.800 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE65.0 DEG CELSIUS
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT0.53 INPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT1.06
INTERAXIS ERROR ANGULAR RANGE IN MINUTESM5.0/P5.0
OUTPUT VOLTAGE FUNCTIONAL ERROR RANGE IN PERCENTM0.2/P0.2
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS0.80 INCH-OUNCES MAXIMUM
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS0.40 INCH-OUNCES MAXIMUM
BODY STYLE STANDARD ROUND D
SHOULDER DIAMETER1.9850 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM
PILOT DIAMETER0.5900 INCHES MINIMUM AND 0.6000 INCHES MAXIMUM
SECOND SHOULDER DIAMETER1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM
SECOND SHOULDER LENGTH0.1700 INCHES NOMINAL
OVERALL LENGTH4.4930 INCHES MINIMUM AND 4.5440 INCHES MAXIMUM
FLANGE DIAMETER2.2490 INCHES MINIMUM AND 2.2500 INCHES MAXIMUM
FLANGE THICKNESS0.2480 INCHES MINIMUM AND 0.2500 INCHES MAXIMUM
BODY DIAMETER1.9850 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM
PILOT LENGTH0.0460 INCHES NOMINAL
SHOULDER LENGTH0.2520 INCHES NOMINAL
AFT OF FIRST FLANGE DIAMETER1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM
MOUNTING SURFACE TO TERMINAL END DISTANCE3.4300 INCHES MINIMUM AND 3.4450 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY7 SCREW
TERMINAL LOCATION REAR
BODY MATERIAL ALUMINUM
TEST DATA DOCUMENT81349-MIL-R-14346 SPECIFICATION (INCLUDES ENGINEERING TYPE BULLETINS, BROCHURES,ETC., THAT REFLECT SPECIFICATION TYPE DATA IN SPECIFICATION FORMAT; EXCLUDES COMMERCIAL CATALOGS, INDUSTRY DIRECTORIES, AND SIMILAR TRADE PUBLICATIONS, REFLECTING GENERAL TYPE DATA ON CERTAIN ENVIRONMENTAL AND PERFORMANCE REQUIREMENTS AND TEST CONDITIONS THAT ARE SHOWN AS "TYPICAL", "AVERAGE", "NOMINAL", ETC.).