NSN 5990-00-902-2663
Part Details | TRANSMITTER SYNCHRO
5990-00-902-2663 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: 14142901, 141429-01, 5990-00-902-2663, 00-902-2663, 5990009022663, 009022663
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1960 | 00-902-2663 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-902-2663
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 141429-01 | 35351 | GE AVIATION SYSTEMS LLC |
Technical Data | NSN 5990-00-902-2663
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 22 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 1.1 AMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 4.4 WATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 3.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 29.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 0.60 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 4.80 NOMINAL |
| ZRS RESISTANCE IN OHMS | 1.30 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 1.70 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 0.50 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 0.21 NOMINAL |
| TRANSFORMATION RATIO | 0.454 STATOR TO ROTOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 1.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 75.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 125.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M10.0/P10.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 49.50 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 18.00 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 2.0000 INCHES NOMINAL |
| PILOT DIAMETER | 0.7495 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
| OVERALL LENGTH | 3.2000 INCHES NOMINAL |
| FLANGE DIAMETER | 2.1600 INCHES MINIMUM AND 2.1610 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.1250 INCHES NOMINAL |
| UNDERCUT DIAMETER | 2.0050 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0950 INCHES NOMINAL |
| PILOT LENGTH | 0.0600 INCHES NOMINAL |
| SHOULDER LENGTH | 0.2000 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 2.6400 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| FRAGILITY FACTOR | MODERATELY RUGGED |
