NSN 5990-00-963-1799
Part Details | TRANSMITTER SYNCHRO
5990-00-963-1799 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: 25794821, 2579482-1, CGJ10WS1A317, CL40912008, 40733502, 4073-35-02, CG10WS1A317, CG-10-WS-1/A317, CG10WS1A317, CG-10-WS-1/A317, 5990-00-963-1799, 00-963-1799, 5990009631799, 009631799
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | JUN 01, 1966 | 00-963-1799 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C

Cross Reference | NSN 5990-00-963-1799
Part Number | Cage Code | Manufacturer |
---|---|---|
2579482-1 | 07187 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
CGJ10WS1A317 | 07187 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
CL40912008 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
4073-35-02 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
CG-10-WS-1/A317 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
CG-10-WS-1/A317 | 4H618 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-963-1799
Characteristic | Specifications |
---|---|
BODY SIZE | 10 |
ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
ROTOR INPUT CURRENT RATING | 20.0 MILLIAMPERES NOMINAL |
ROTOR INPUT ELECTRICAL POWER RATING | 1.0 WATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ZRO RESISTANCE IN OHMS | 25.00 NOMINAL |
PLUS J ZRO REACTANCE IN OHMS | 128.00 NOMINAL |
ZSO RESISTANCE IN OHMS | 6.40 NOMINAL |
PLUS J ZSO REACTANCE IN OHMS | 23.00 NOMINAL |
ZRS RESISTANCE IN OHMS | 41.00 NOMINAL |
PLUS J ZRS REACTANCE IN OHMS | 14.00 NOMINAL |
ROTOR DC RESISTANCE IN OHMS | 15.00 NOMINAL |
STATOR DC RESISTANCE IN OHMS | 6.50 NOMINAL |
TRANSFORMATION RATIO | 0.454 STATOR TO ROTOR NOMINAL |
PHASE SHIFT ANGLE IN DEG | 7.000 INPUT TO OUTPUT NOMINAL |
MAXIMUM TEMP RISE | 30.0 DEG CELSIUS |
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M6.0/P6.0 |
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.0 CENTIMETER-GRAMS NOMINAL |
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS NOMINAL |
TORQUE GRADIENT PER ANGULAR DEG | 3400.0 MILLIMETER-MILLIGRAMS NOMINAL |
BODY STYLE | STANDARD ROUND C |
SHOULDER DIAMETER | 0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM |
PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
OVERALL LENGTH | 1.7210 INCHES NOMINAL |
FLANGE DIAMETER | 0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM |
FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
UNDERCUT DIAMETER | 0.8400 INCHES NOMINAL |
UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
PILOT LENGTH | 0.0380 INCHES NOMINAL |
SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2460 INCHES MAXIMUM |
ALIGNMENT HOLE DEPTH | 0.3750 INCHES NOMINAL |
ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.6780 INCHES NOMINAL |
ALIGNMENT HOLE QUANTITY | 3 |
TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
TERMINAL LOCATION | REAR |
BODY MATERIAL | STEEL, CORROSION RESISTING |
FRAGILITY FACTOR | MODERATELY RUGGED |