NSN 5990-00-018-8604

Part Details | TRANSMITTER SYNCHRO

5990-00-018-8604 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: 11TX300N22A10, 11TX-300-N-22A/10, U214778, U-214778, 617461, SMC617461, SMC617461, SM-C-617461, 5990-00-018-8604, 00-018-8604, 5990000188604, 000188604

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59MAY 15, 196800-018-860402073 ( SYNCHRO, TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

1 Y-ROTOR, 1 STATOR

Cross Reference | NSN 5990-00-018-8604
Part Number Cage Code Manufacturer
11TX-300-N-22A/1006989API HAROWE INCDBA API MOTION DIV API
U-21477882686TRANSICOIL LLCDBA ADS/TRANSICOIL
61746136180ULTRA ELECTRONICS MARITIMESYSTEMSINC DBA ULTRA
SMC61746136180ULTRA ELECTRONICS MARITIMESYSTEMSINC DBA ULTRA
SM-C-61746180063US ARMY COMMUNICATIONS &ELECTRONICS MATERIEL READINESS
Technical Data | NSN 5990-00-018-8604
Characteristic Specifications
BODY SIZE11
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
ROTOR INPUT CURRENT RATING173.0 MILLIAMPERES MAXIMUM
ROTOR INPUT ELECTRICAL POWER RATING800.0 MILLIWATTS MAXIMUM
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS29.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS163.00 NOMINAL
ZRS RESISTANCE IN OHMS43.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS15.00 NOMINAL
ZSS RESISTANCE IN OHMS6.00 NOMINAL
PLUS J ZSS REACTANCE IN OHMS27.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS19.00 NOMINAL
STATOR DC RESISTANCE IN OHMS6.00 NOMINAL
TRANSFORMATION RATIO0.454 ROTOR TO STATOR NOMINAL
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM10.0/P10.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS15.0 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS3.0 CENTIMETER-GRAMS NOMINAL
TORQUE GRADIENT PER ANGULAR DEG3500.0 MILLIMETER-MILLIGRAMS MINIMUM
BODY STYLE STANDARD ROUND C
SHOULDER DIAMETER1.0000 INCHES MAXIMUM
PILOT DIAMETER0.6250 INCHES MAXIMUM
OVERALL LENGTH2.2170 INCHES MAXIMUM
FLANGE DIAMETER1.0620 INCHES MAXIMUM
FLANGE THICKNESS0.0930 INCHES NOMINAL
UNDERCUT DIAMETER0.9750 INCHES NOMINAL
UNDERCUT WIDTH0.0620 INCHES MINIMUM
PILOT LENGTH0.0620 INCHES NOMINAL
SHOULDER LENGTH0.0620 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.6400 INCHES MAXIMUM
ALIGNMENT HOLE DEPTH0.0500 INCHES MAXIMUM
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.8120 INCHES MINIMUM
ALIGNMENT HOLE QUANTITY4
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL ALUMINUM ALLOY
SHAFT MAXIMUM RADIAL PLAY0.0008 INCHES
SHAFT RADIAL PLAY TEST POINT0.125 INCHES NOMINAL
SHAFT RADIAL PLAY DETERMINING WEIGHT4.0 OUNCES
SHAFT END PLAY0.0010 INCHES NOMINAL
SHAFT END PLAY DETERMINING WEIGHT4.0 OUNCES
SHAFT MAXIMUM RUNOUT0.0010 INCHES
SCHEMATIC DIAGRAM DESIGNATOR 1 Y-ROTOR, 1 STATOR
FRAGILITY FACTOR MODERATELY RUGGED