NSN 5990-00-780-8915

Part Details | ELECTRICAL RESOLVER

5990-00-780-8915 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: 11R2NUR100X, 11R2N4R100X, MILR2153014, MILR21530-14, 2258821, 5990-00-780-8915, 00-780-8915, 5990007808915, 007808915

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59MAR 22, 196800-780-891522966 ( RESOLVER, ELECTRICAL )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

Cross Reference | NSN 5990-00-780-8915
Part Number Cage Code Manufacturer
11R2NUR100XC2786ACUTRONIC DEUTSCHLAND GMBH
11R2N4R100X81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MILR21530-1481349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
225882110001NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT
Technical Data | NSN 5990-00-780-8915
Characteristic Specifications
BODY SIZE11
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
ROTOR INPUT CURRENT RATING145.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING760.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS36.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS175.00 NOMINAL
ZSO RESISTANCE IN OHMS7.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS41.50 NOMINAL
ZRS RESISTANCE IN OHMS38.50 NOMINAL
PLUS J ZRS REACTANCE IN OHMS17.80 NOMINAL
ZSS RESISTANCE IN OHMS9.30 NOMINAL
PLUS J ZSS REACTANCE IN OHMS4.70 NOMINAL
TRANSFORMATION RATIO0.454 STATOR TO ROTOR NOMINAL
PHASE SHIFT ANGLE IN DEG7.000 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE20.0 DEG CELSIUS
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT20.00 OUTPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT30.00
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS25.0 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS15.0 CENTIMETER-GRAMS NOMINAL
BODY STYLE STANDARD ROUND C
SHOULDER DIAMETER0.9997 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM
PILOT DIAMETER0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM
OVERALL LENGTH2.4620 INCHES MAXIMUM
FLANGE DIAMETER1.0570 INCHES MINIMUM AND 1.0750 INCHES MAXIMUM
FLANGE THICKNESS0.0900 INCHES MINIMUM AND 0.0960 INCHES MAXIMUM
UNDERCUT DIAMETER0.9750 INCHES NOMINAL
UNDERCUT WIDTH0.0570 INCHES MINIMUM AND 0.0670 INCHES MAXIMUM
PILOT LENGTH0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM
SHOULDER LENGTH0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM
MOUNTING SURFACE TO TERMINAL END DISTANCE1.8600 INCHES MAXIMUM
ALIGNMENT HOLE DEPTH0.1250 INCHES NOMINAL
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.8120 INCHES NOMINAL
ALIGNMENT HOLE QUANTITY4
TERMINAL TYPE AND QUANTITY8 SCREW
TERMINAL LOCATION REAR
BODY MATERIAL ALUMINUM
TEST DATA DOCUMENT81349-MIL-R-21530 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.).