NSN 5990-01-054-4255

Part Details | TRANSMITTER SYNCHRO

5990-01-054-4255 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: VCDX156N3, VCDX15-6N3, 15CDX6C, M207082202C, M20708/22-02C, MILS2070822, MIL-S-20708/22, 5990-01-054-4255, 01-054-4255, 5990010544255, 010544255

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 20, 197801-054-425502073 ( SYNCHRO, TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND B

Cross Reference | NSN 5990-01-054-4255
Part Number Cage Code Manufacturer
VCDX15-6N310112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
15CDX6C81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/22-02C81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-20708/2281349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
Technical Data | NSN 5990-01-054-4255
Characteristic Specifications
BODY SIZE15
ROTOR INPUT VOLTAGE RATING IN VOLTS90.0 NOMINAL
ROTOR INPUT CURRENT RATING38.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING500.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZSO RESISTANCE IN OHMS2050.00 MINIMUM AND 2600.00 MAXIMUM
PLUS J ZSO REACTANCE IN OHMS77.00 MINIMUM AND 83.00 MAXIMUM
ZRS RESISTANCE IN OHMS900.00 MINIMUM AND 1200.00 MAXIMUM
ZSO-90 RESISTANCE IN OHMS2050.00 MINIMUM AND 2600.00 MAXIMUM
TRANSFORMATION RATIO1.154 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG9.000 INPUT TO OUTPUT NOMINAL
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT60.00 INPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT100.00
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS20.00 INCH-OUNCES NOMINAL
BODY STYLE STANDARD ROUND B
SHOULDER DIAMETER1.3120 INCHES NOMINAL
PILOT DIAMETER0.8750 INCHES NOMINAL
OVERALL LENGTH3.2170 INCHES MAXIMUM
FLANGE DIAMETER1.4370 INCHES NOMINAL
FLANGE THICKNESS0.0930 INCHES NOMINAL
UNDERCUT WIDTH0.0780 INCHES NOMINAL
PILOT LENGTH0.0400 INCHES NOMINAL
SHOULDER LENGTH0.1320 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE2.6770 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY5 SCREW
TERMINAL LOCATION REAR
BODY MATERIAL ALUMINUM ALLOY
TEST DATA DOCUMENT81349-MILS20708 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 22 GOVERNMENT SPECIFICATION
FRAGILITY FACTOR MODERATELY RUGGED