NSN 5990-00-457-8940

Part Details | ELECTRICAL RESOLVER

5990-00-457-8940 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: ESH11CJS5F211, ESH-11-CJS-5/F211, ESH11CJS5B548, ESH-11-CJS-5/B548, 10189018, 10056488, 10189018, 10189018, 5990-00-457-8940, 00-457-8940, 5990004578940, 004578940

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59APR 30, 196900-457-894022966 ( RESOLVER, ELECTRICAL )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND B

RESOLVER,ELECTRICAL | 5990-00-457-8940, 004578940

2 ROTOR, 2 STATOR

RESOLVER,ELECTRICAL | 5990-00-457-8940, 004578940
Cross Reference | NSN 5990-00-457-8940
Part Number Cage Code Manufacturer
ESH-11-CJS-5/F21199932MOOG INC.DBA MOOG COMPONENTS GROUP
ESH-11-CJS-5/B54899932MOOG INC.DBA MOOG COMPONENTS GROUP
101890182X130MOTION DEVICES TECHNOLOGY, INC.
10056488A486GNIMIKKEISTOKESKUS NCB FINLAND
1018901882686TRANSICOIL LLCDBA ADS/TRANSICOIL
1018901818876U S ARMY AVIATION AND MISSILECOMMAND
Technical Data | NSN 5990-00-457-8940
Characteristic Specifications
BODY SIZE11
BODY STYLE STANDARD ROUND B
SHOULDER DIAMETER0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM
PILOT DIAMETER0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM
OVERALL LENGTH2.1470 INCHES NOMINAL
FLANGE DIAMETER1.0620 INCHES NOMINAL
FLANGE THICKNESS0.0930 INCHES NOMINAL
UNDERCUT WIDTH0.0500 INCHES NOMINAL
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 DISTANCE1.8350 INCHES NOMINAL
TERMINAL TYPE AND QUANTITY7 SCREW
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, STAINLESS
SCHEMATIC DIAGRAM DESIGNATOR3 2 ROTOR, 2 STATOR
FRAGILITY FACTOR MODERATELY RUGGED