NSN 5990-00-206-3753

Part Details | TRANSMITTER SYNCHRO


5990-00-206-3753 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: VCX114G1, VCX11-4G1, 011702M1, 011-702M1, 11CX4E, 011702M1, 011-702M1, M207082C005, M20708/2C-005, M20708205E, M20708/2-05E, M207082005, M20708/2-005, MILS207082, MIL-S-20708/2, 11CX4E, 11CX4E, 1.791521, 59 00013, 59 000-13, AS207082, AS20708/2, 5990-00-206-3753, 00-206-3753, 5990002063753, 002063753

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59APR 13, 197300-206-375302073 ( SYNCHRO, TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C


Cross Reference | NSN 5990-00-206-3753
Part Number Cage Code Manufacturer
VCX11-4G110112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
011-702M199743IMC MAGNETICS CORPWESTERN DIV
11CX4E88818KEARFOTT CORPORATIONDBA KEARFOTT
011-702M192703KEMTRON ELECTRON PRODUCTS INC
M20708/2C-00581349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/2-05E81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/2-00581349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-20708/281349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
11CX4E81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
11CX4E99932MOOG INC.DBA MOOG COMPONENTS GROUP
1.791521D2865RAYTHEON ANSCHUETZ GMBHDBA RAYTHEON ELECTRICS GMBH
59 000-13D9853ROCKWELL COLLINS DEUTSCHLANDSERVICES GMBH
AS20708/20VH01SAE CUSTOMER SERVICEDEPT 2045

Technical Data | NSN 5990-00-206-3753
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 RESISTANCE IN OHMS3720.00 MINIMUM AND 4700.00 MAXIMUM
ZSS RESISTANCE IN OHMS410.00 MINIMUM AND 500.00 MAXIMUM
ZRO IMPEDANCE MAGNITUDE IN OHMS80.00 MINIMUM AND 84.00 MAXIMUM
ZSS IMPEDANCE MAGNITUDE IN OHMS17.00 MINIMUM AND 26.00 MAXIMUM
TRANSFORMATION RATIO0.783 ROTOR TO STATOR 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 MINUS 55 DEG CELSIUS0.07 INCH-OUNCES MAXIMUM
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 LENGTH2.3360 INCHES MINIMUM AND 2.3760 INCHES MAXIMUM
FLANGE DIAMETER1.0570 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM
FLANGE THICKNESS0.0930 INCHES NOMINAL
UNDERCUT DIAMETER0.9750 INCHES NOMINAL
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0450 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM
SHOULDER LENGTH0.0590 INCHES MINIMUM AND 0.0790 INCHES MAXIMUM
MOUNTING SURFACE TO TERMINAL END DISTANCE1.7910 INCHES MINIMUM AND 1.8110 INCHES MAXIMUM
ALIGNMENT HOLE DEPTH0.1250 INCHES NOMINAL
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.6250 INCHES NOMINAL
SECURING HOLE QUANTITY4
MOUNTING FACILITY SCREW THREAD SERIES DESIGNATOR UNC
MOUNTING FACILITY NOMINAL SCREW THREAD DIAMETER0.112 INCHES
TERMINAL TYPE AND QUANTITY5 SCREW
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, STAINLESS
TEST DATA DOCUMENT81349-MIL-S-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.).
FRAGILITY FACTOR MODERATELY RUGGED