NSN 5990-00-677-6496

Part Details | CONTROL TRANSFORMER SYNCHRO

5990-00-677-6496 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: 23CT6C, 23CT6C, MILS2070853, MIL-S-20708/53, 23CT6C, 23CT6C, 23CT6C, 5990-00-677-6496, 00-677-6496, 5990006776496, 006776496

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 21, 197800-677-649615289 ( SYNCHRO, CONTROL TRANSFORMER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND D

Cross Reference | NSN 5990-00-677-6496
Part Number Cage Code Manufacturer
23CT6CD1901HENSOLDT SENSORS GMBHDIV SEPS
23CT6C81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-20708/5381349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
23CT6CS0514SAFT AB
23CT6CA145NSAFT AB
23CT6C10651VERNITRON CORP
Technical Data | NSN 5990-00-677-6496
Characteristic Specifications
BODY SIZE23
STATOR INPUT VOLTAGE RATING IN VOLTS90.0 NOMINAL
STATOR INPUT CURRENT RATING20.0 MILLIAMPERES NOMINAL
STATOR INPUT ELECTRICAL POWER RATING450.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ60.0 NOMINAL
ZSO IMPEDANCE MAGNITUDE IN OHMS4200.00 MINIMUM AND 5100.00 MAXIMUM
ZSO IMPEDANCE ANGLE IN DEG70.00 MINIMUM AND 76.00 MAXIMUM
ZRS IMPEDANCE MAGNITUDE IN OHMS1350.00 MINIMUM AND 1650.00 MAXIMUM
ZRS IMPEDANCE ANGLE IN DEG14.00 MINIMUM AND 20.00 MAXIMUM
TRANSFORMATION RATIO0.735 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG14.000 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE10.0 DEG CELSIUS
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM6.0/P6.0
TORQUE GRADIENT PER ANGULAR DEG0.2 MILLIMETER-MILLIGRAMS NOMINAL
BODY STYLE STANDARD ROUND D
SHOULDER DIAMETER1.9900 INCHES NOMINAL
PILOT DIAMETER0.6000 INCHES NOMINAL
SECOND SHOULDER DIAMETER1.9995 INCHES NOMINAL
SECOND SHOULDER LENGTH0.1700 INCHES NOMINAL
OVERALL LENGTH4.2990 INCHES NOMINAL
FLANGE DIAMETER2.2500 INCHES NOMINAL
FLANGE THICKNESS2.5000 INCHES NOMINAL
PILOT LENGTH0.0430 INCHES NOMINAL
SHOULDER LENGTH0.2500 INCHES NOMINAL
TERMINAL TYPE AND QUANTITY5 SCREW
TERMINAL LOCATION REAR
BODY MATERIAL ANY ACCEPTABLE