NSN 5990-00-254-4825

Part Details | CONTROL TRANSFORMER SYNCHRO

5990-00-254-4825 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the rotor is dependent upon both the position of the rotor and the electrical input to the stator from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, or variable transformers.

Alternate Parts: VCT156N2, VCT15-6N2, CT156N3, CT15-6N3, 15CT6D, M2070821D002, M20708/21D-002, M207082102D, M20708/21-02D, MILS2070821D002, MILS20708-21D002, MILS2070821, MIL-S-20708/21, AS2070821, AS20708/21, AS2070821, AS20708/21, M207082102S, M20708/21-02S, 5990-00-254-4825, 00-254-4825, 5990002544825, 002544825

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JUN 18, 197300-254-482515289 ( SYNCHRO, CONTROL TRANSFORMER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND B

SYNCHRO,CONTROL TRA | 5990-00-254-4825, 002544825
Cross Reference | NSN 5990-00-254-4825
Part Number Cage Code Manufacturer
VCT15-6N210112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
CT15-6N310112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
15CT6D81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/21D-00281349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/21-02D81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MILS20708-21D00281349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-20708/2181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
AS20708/210VH01SAE CUSTOMER SERVICEDEPT 2045
AS20708/2181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
M20708/21-02S81343SOCIETY OF AUTOMOTIVE ENGINEERS INC
Technical Data | NSN 5990-00-254-4825
Characteristic Specifications
BODY SIZE15
STATOR INPUT VOLTAGE RATING IN VOLTS90.0 NOMINAL
STATOR INPUT CURRENT RATING13.0 MILLIAMPERES NOMINAL
STATOR INPUT ELECTRICAL POWER RATING210.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ60.0 NOMINAL
ZSO RESISTANCE IN OHMS6000.00 MINIMUM AND 7500.00 MAXIMUM
ZRS RESISTANCE IN OHMS1300.00 MINIMUM AND 1650.00 MAXIMUM
ZSO IMPEDANCE MAGNITUDE IN OHMS78.00 MINIMUM AND 82.00 MAXIMUM
ZRS IMPEDANCE MAGNITUDE IN OHMS13.00 MINIMUM AND 18.00 MAXIMUM
TRANSFORMATION RATIO0.735 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG9.000 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE10.0 DEG CELSIUS
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT45.00 OUTPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT65.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM6.0/P6.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS0.05 INCH-OUNCES MAXIMUM
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS0.05 INCH-OUNCES MAXIMUM
BODY STYLE STANDARD ROUND B
SHOULDER DIAMETER1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM
PILOT DIAMETER0.8745 INCHES MINIMUM AND 0.8750 INCHES MAXIMUM
OVERALL LENGTH3.0430 INCHES MINIMUM AND 3.0830 INCHES MAXIMUM
FLANGE DIAMETER1.4320 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM
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 DISTANCE2.3910 INCHES MAXIMUM
ALIGNMENT HOLE DEPTH0.1250 INCHES NOMINAL
ALIGNMENT HOLE BOLT CIRCLE DIAMETER1.0970 INCHES MINIMUM AND 1.1030 INCHES MAXIMUM
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.).
SPECIFICATION/STANDARD DATA81349-MIL--20708 TO 21 GOVERNMENT SPECIFICATION
FRAGILITY FACTOR MODERATELY RUGGED