NSN 5990-00-754-8068

Part Details | TRANSMITTER SYNCHRO

5990-00-754-8068 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: GA10025L1, GA10025L1, 6010323, 3075713, 307571-3, 10351578, R2101AA, R210-1AA, R2101A, R210-1A, R2101, R210-1, 10351578, 1JC78946, 1JC7894-6, 1JC17541, 1JC1754-1, 9904501, 990450-1, 191109, 10351578, 10351578, 10351578, 1JC78946, 1JC7894-6, 1JC17541, 1JC1754-1, 5990-00-754-8068, 00-754-8068, 5990007548068, 007548068

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 01, 196200-754-806802073 ( SYNCHRO, TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

Cross Reference | NSN 5990-00-754-8068
Part Number Cage Code Manufacturer
GA10025L164959AMERICAN TELEPHONE AND TELEGRAPH CO
GA10025L170408AT AND T CORP
601032381891INTERNATIONAL BUSINESS MACHINES CORP
307571-388818KEARFOTT CORPORATIONDBA KEARFOTT
1035157888818KEARFOTT CORPORATIONDBA KEARFOTT
R210-1AA88818KEARFOTT CORPORATIONDBA KEARFOTT
R210-1A88818KEARFOTT CORPORATIONDBA KEARFOTT
R210-188818KEARFOTT CORPORATIONDBA KEARFOTT
1035157897942NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN SYSTEMS
1JC7894-697942NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN SYSTEMS
1JC1754-197942NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN SYSTEMS
990450-182577RAYTHEON COMPANYDBA RAYTHEON
19110937695RAYTHEON COMPANYDBA RAYTHEON
1035157882577RAYTHEON COMPANYDBA RAYTHEON
1035157818876U S ARMY AVIATION AND MISSILECOMMAND
1035157879500WESTINGHOUSE ELECTRIC CORP
1JC7894-679500WESTINGHOUSE ELECTRIC CORP
1JC1754-179500WESTINGHOUSE ELECTRIC CORP
Technical Data | NSN 5990-00-754-8068
Characteristic Specifications
BODY SIZE11
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
ROTOR INPUT CURRENT RATING209.0 MILLIAMPERES MAXIMUM
ROTOR INPUT ELECTRICAL POWER RATING960.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO IMPEDANCE MAGNITUDE IN OHMS150.00 NOMINAL
ZRO IMPEDANCE ANGLE IN DEG78.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS16.00 NOMINAL
STATOR DC RESISTANCE IN OHMS5.00 NOMINAL
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT35.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM10.0/P10.0
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS4.0 CENTIMETER-GRAMS MAXIMUM
TORQUE GRADIENT PER ANGULAR DEG2000.0 MILLIMETER-MILLIGRAMS MINIMUM
BODY STYLE STANDARD ROUND C
SHOULDER DIAMETER0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM
PILOT DIAMETER0.5000 INCHES NOMINAL
OVERALL LENGTH2.1830 INCHES NOMINAL
FLANGE DIAMETER1.0570 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM
FLANGE THICKNESS0.0620 INCHES NOMINAL
UNDERCUT DIAMETER0.9620 INCHES NOMINAL
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0620 INCHES NOMINAL
SHOULDER LENGTH0.0620 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.8010 INCHES NOMINAL
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, CORROSION RESISTING