NSN 5990-00-099-0700

Part Details | ELECTRICAL RESOLVER


5990-00-099-0700 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: 9V11R41N40A, 9V-11R41N40A, MILR2341725, MIL-R-23417/25, 5990-00-099-0700, 00-099-0700, 5990000990700, 000990700

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59DEC 13, 197200-099-070022966 ( RESOLVER, ELECTRICAL )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C


Cross Reference | NSN 5990-00-099-0700
Part Number Cage Code Manufacturer
9V-11R41N40A81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-R-23417/2581349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY

Technical Data | NSN 5990-00-099-0700
Characteristic Specifications
BODY SIZE11
ROTOR INPUT VOLTAGE RATING IN VOLTS9.0 NOMINAL
ROTOR INPUT CURRENT RATING2.6 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING10.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ4000.0 NOMINAL
ZRO RESISTANCE IN OHMS3720.00 MINIMUM AND 4467.00 MAXIMUM
ZSS RESISTANCE IN OHMS121.00 MINIMUM AND 145.00 MAXIMUM
ZRO IMPEDANCE MAGNITUDE IN OHMS68.00 MINIMUM AND 73.00 MAXIMUM
ZSS IMPEDANCE MAGNITUDE IN OHMS65.00 MINIMUM AND 69.00 MAXIMUM
TRANSFORMATION RATIO0.497 ROTOR TO STATOR NOMINAL
MAXIMUM TEMP RISE85.0 DEG CELSIUS
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT15.00 OUTPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT20.00
INTERAXIS ERROR ANGULAR RANGE IN MINUTESM7.0/P7.0
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 LENGTH2.4130 INCHES MAXIMUM
FLANGE DIAMETER1.0570 INCHES MINIMUM AND 1.0650 INCHES MAXIMUM
FLANGE THICKNESS0.0930 INCHES NOMINAL
UNDERCUT DIAMETER0.9745 INCHES MINIMUM AND 0.9750 INCHES MAXIMUM
UNDERCUT WIDTH0.0500 INCHES NOMINAL
PILOT LENGTH0.0620 INCHES NOMINAL
SHOULDER LENGTH0.0620 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE2.3340 INCHES MINIMUM AND 2.3540 INCHES MAXIMUM
ALIGNMENT HOLE DEPTH0.1250 INCHES NOMINAL
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.8090 INCHES MINIMUM AND 0.8150 INCHES MAXIMUM
ALIGNMENT HOLE QUANTITY4
TERMINAL TYPE AND QUANTITY7 SCREW
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, STAINLESS
TEST DATA DOCUMENT81349-MIL-R-23417 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.).
SPECIFICATION/STANDARD DATA81349-MIL-R-23417 TO 25 GOVERNMENT SPECIFICATION