NSN 5990-00-477-1362

Part Details | TRANSMITTER SYNCHRO

5990-00-477-1362 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the stator into a receiver synchro, a control transformer or differential synchro is dependent upon the position of its rotor. Does not include variable resistors, goniometers, variable transformers, or items with dials.

Alternate Parts: 11CX13464, 11CX1346-4, CR40913002, 11CX4E, M20708204E, M20708/2-04E, MILS207082, MIL-S-20708/2, AS207082, AS20708/2, 5990-00-477-1362, 00-477-1362, 5990004771362, 004771362

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JUN 18, 197100-477-136202073 ( SYNCHRO, TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

Cross Reference | NSN 5990-00-477-1362
Part Number Cage Code Manufacturer
11CX1346-414404AMETEK TECHNICAL & INDUSTRIALPRODUCTS, INC.
CR4091300205088KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS
11CX4E81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/2-04E81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-20708/281349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
AS20708/20VH01SAE CUSTOMER SERVICEDEPT 2045
Technical Data | NSN 5990-00-477-1362
Characteristic Specifications
BODY SIZE11
ROTOR INPUT VOLTAGE RATING IN VOLTS115.0 NOMINAL
ROTOR INPUT CURRENT RATING31.0 MILLIAMPERES MAXIMUM
ROTOR INPUT ELECTRICAL POWER RATING490.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO IMPEDANCE MAGNITUDE IN OHMS3720.00 MINIMUM AND 4700.00 MAXIMUM
ZRO IMPEDANCE ANGLE IN DEG80.00 MINIMUM AND 84.00 MAXIMUM
ZSS IMPEDANCE MAGNITUDE IN OHMS410.00 MINIMUM AND 500.00 MAXIMUM
ZSS IMPEDANCE ANGLE IN DEG17.00 MINIMUM AND 26.00 MAXIMUM
TRANSFORMATION RATIO0.783 STATOR TO ROTOR NOMINAL
PHASE SHIFT ANGLE IN DEG4.500 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE20.0 DEG CELSIUS
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT45.00 OUTPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT75.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM7.0/P7.0
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS0.07 INCH-OUNCES MAXIMUM
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 LENGTH2.2930 INCHES NOMINAL
FLANGE DIAMETER1.0575 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM
FLANGE THICKNESS0.0930 INCHES NOMINAL
UNDERCUT DIAMETER0.9750 INCHES NOMINAL
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0620 INCHES NOMINAL
SHOULDER LENGTH0.0620 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.7940 INCHES NOMINAL
ALIGNMENT HOLE DEPTH0.1250 INCHES MINIMUM
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.8120 INCHES NOMINAL
ALIGNMENT HOLE QUANTITY4
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, CORROSION RESISTING
TEST DATA DOCUMENT81349-MILS-20708 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--20708 TO 2 GOVERNMENT SPECIFICATION
FRAGILITY FACTOR MODERATELY RUGGED