NSN 5990-01-042-1984

Part Details | CONTROL TRANSFORMER SYNCHRO

5990-01-042-1984 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: 2692782, 2692782, 15CT4, VCT154M2, VCT15-4M2, 2692782, 5990-01-042-1984, 01-042-1984, 5990010421984, 010421984

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JUN 07, 197701-042-198415289 ( SYNCHRO, CONTROL TRANSFORMER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND B

Cross Reference | NSN 5990-01-042-1984
Part Number Cage Code Manufacturer
269278244114BAE SYSTEMS LAND & ARMAMENTS L.P.
269278210112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
15CT410112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
VCT15-4M210112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
269278210001NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT
Technical Data | NSN 5990-01-042-1984
Characteristic Specifications
BODY SIZE15
STATOR INPUT VOLTAGE RATING IN VOLTS11.8 NOMINAL
STATOR INPUT CURRENT RATING1.31 MILLIAMPERES NOMINAL
STATOR INPUT ELECTRICAL POWER RATING2.4 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZSO IMPEDANCE MAGNITUDE IN OHMS7800.00 MINIMUM AND 9512.00 MAXIMUM
ZSO IMPEDANCE ANGLE IN DEG78.80 MINIMUM AND 84.50 MAXIMUM
ZRS IMPEDANCE MAGNITUDE IN OHMS1050.00 MINIMUM AND 1300.00 MAXIMUM
ZRS IMPEDANCE ANGLE IN DEG26.00 MINIMUM AND 33.00 MAXIMUM
PHASE SHIFT ANGLE IN DEG5.500 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE10.0 DEG CELSIUS
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT4.19 OUTPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT7.86
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM6.0/P6.0
BODY STYLE STANDARD ROUND B
SHOULDER DIAMETER1.3120 INCHES NOMINAL
PILOT DIAMETER0.8750 INCHES NOMINAL
OVERALL LENGTH2.3220 INCHES MAXIMUM
FLANGE DIAMETER1.4370 INCHES NOMINAL
FLANGE THICKNESS0.0930 INCHES NOMINAL
UNDERCUT WIDTH0.0780 INCHES NOMINAL
PILOT LENGTH0.0400 INCHES NOMINAL
SHOULDER LENGTH0.1320 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.6400 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY5 SCREW
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, STAINLESS
FRAGILITY FACTOR MODERATELY RUGGED