NSN 5990-00-675-4567

Part Details | TRANSMITTER SYNCHRO

5990-00-675-4567 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: SGC29C4A223, 9001330005, 900133-0005, 9001335, 900133-5, 5990-00-675-4567, 00-675-4567, 5990006754567, 006754567

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 01, 196300-675-456702073 ( SYNCHRO, TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND A

1 Y-ROTOR, 1 STATOR

Cross Reference | NSN 5990-00-675-4567
Part Number Cage Code Manufacturer
SGC29C4A22399932MOOG INC.DBA MOOG COMPONENTS GROUP
900133-000506481NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS
900133-506481NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS
Technical Data | NSN 5990-00-675-4567
Characteristic Specifications
BODY SIZE20
ROTOR INPUT VOLTAGE RATING IN VOLTS15.0 NOMINAL
ROTOR INPUT CURRENT RATING28.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING200.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ5000.0 NOMINAL
ZRO IMPEDANCE MAGNITUDE IN OHMS536.00 NOMINAL
ZRO IMPEDANCE ANGLE IN DEG68.00 NOMINAL
ZSO IMPEDANCE MAGNITUDE IN OHMS270.00 NOMINAL
ZSO IMPEDANCE ANGLE IN DEG66.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS20.00 NOMINAL
STATOR DC RESISTANCE IN OHMS32.00 NOMINAL
PHASE SHIFT ANGLE IN DEG5.000 INPUT TO OUTPUT MAXIMUM
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT9.00 INPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT18.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM30.0/P30.0
BODY STYLE3 STANDARD ROUND A
OVERALL LENGTH0.8500 INCHES NOMINAL
BODY DIAMETER2.0000 INCHES NOMINAL
BODY THRU-HOLE DIAMETER0.5450 INCHES NOMINAL
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
TERMINAL LOCATION SIDE
BODY MATERIAL STEEL, CORROSION RESISTING
SPECIAL FEATURESLEADS 15 IN. MIN LG
SCHEMATIC DIAGRAM DESIGNATOR 1 Y-ROTOR, 1 STATOR
FRAGILITY FACTOR MODERATELY RUGGED