NSN 5990-00-910-4500

Part Details | CONTROL TRANSFORMER SYNCHRO

5990-00-910-4500 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: 8CT300A1, 8CT-300-A-1, 327926, 327-926, 327926, 327-926, CTH8A1A013, CTH-8-A1/A013, CTH8A1, CTH-8-A-1, CTC8A1, CMC327926, CMC327-926, 9900016, 990001-6, 5990-00-910-4500, 00-910-4500, 5990009104500, 009104500

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 01, 196000-910-450015289 ( SYNCHRO, CONTROL TRANSFORMER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND A

1 Y-ROTOR, 1 STATOR

Cross Reference | NSN 5990-00-910-4500
Part Number Cage Code Manufacturer
8CT-300-A-106989API HAROWE INCDBA API MOTION DIV API
327-92690073CMC ELECTRONICS INC
327-92699932MOOG INC.DBA MOOG COMPONENTS GROUP
CTH-8-A1/A01399932MOOG INC.DBA MOOG COMPONENTS GROUP
CTH-8-A-199932MOOG INC.DBA MOOG COMPONENTS GROUP
CTC8A199932MOOG INC.DBA MOOG COMPONENTS GROUP
CMC327-92699932MOOG INC.DBA MOOG COMPONENTS GROUP
990001-682577RAYTHEON COMPANYDBA RAYTHEON
Technical Data | NSN 5990-00-910-4500
Characteristic Specifications
BODY SIZE8
STATOR INPUT VOLTAGE RATING IN VOLTS11.8 NOMINAL
STATOR INPUT CURRENT RATING87.0 MILLIAMPERES NOMINAL
STATOR INPUT ELECTRICAL POWER RATING210.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS210.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS690.00 NOMINAL
ZSO RESISTANCE IN OHMS28.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS114.00 NOMINAL
ZRS RESISTANCE IN OHMS250.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS73.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS143.00 NOMINAL
STATOR DC RESISTANCE IN OHMS24.00 NOMINAL
PHASE SHIFT ANGLE IN DEG9.000 OUTPUT TO INPUT NOMINAL
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT30.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM7.0/P7.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS16.0 CENTIMETER-GRAMS MAXIMUM
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS4.0 CENTIMETER-GRAMS MAXIMUM
BODY STYLE STANDARD ROUND A
PILOT DIAMETER0.5000 INCHES MAXIMUM
OVERALL LENGTH1.6360 INCHES MAXIMUM
FLANGE DIAMETER0.7500 INCHES MAXIMUM
FLANGE THICKNESS0.0620 INCHES MAXIMUM
UNDERCUT DIAMETER0.6910 INCHES MAXIMUM
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0430 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2410 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, STAINLESS
SHAFT MAXIMUM RADIAL PLAY0.0005 INCHES
SHAFT RADIAL PLAY TEST POINT0.125 INCHES NOMINAL
SHAFT RADIAL PLAY DETERMINING WEIGHT4.0 OUNCES
SHAFT END PLAY0.0003 INCHES MINIMUM AND 0.0008 INCHES MAXIMUM
SHAFT END PLAY DETERMINING WEIGHT8.0 OUNCES
SHAFT MAXIMUM RUNOUT0.0010 INCHES
SCHEMATIC DIAGRAM DESIGNATOR 1 Y-ROTOR, 1 STATOR
FRAGILITY FACTOR MODERATELY RUGGED