Part Details | TRANSMITTER SYNCHRO
5990-00-715-1492 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: 172097001, 172097-001, 5990-00-715-1492, 00-715-1492, 5990007151492, 007151492
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1961 | 00-715-1492 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
1 Y-ROTOR, 1 STATOR
Cross Reference | NSN 5990-00-715-1492
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 172097-001 | 81413 | BAE SYSTEMS INFORMATION ANDELECTRONIC SYSTEMS INTEGRATION I |
Technical Data | NSN 5990-00-715-1492
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 264.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 1.1 WATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 16.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 107.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 3.70 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 18.10 NOMINAL |
| ZRS RESISTANCE IN OHMS | 22.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 8.90 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 8.50 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 3.00 NOMINAL |
| TRANSFORMATION RATIO | 0.454 STATOR TO ROTOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 5.000 OUTPUT TO INPUT NOMINAL |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 22.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.00 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.00 CENTIMETER-GRAMS MAXIMUM |
| BODY STYLE | STANDARD ROUND B |
| SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 2.1150 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.0590 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
| PILOT LENGTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| SHOULDER LENGTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6000 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| SHAFT MAXIMUM RADIAL PLAY | 0.0008 INCHES |
| SHAFT RADIAL PLAY TEST POINT | 0.125 INCHES NOMINAL |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT END PLAY | 0.0005 INCHES MINIMUM AND 0.0015 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 16.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| SCHEMATIC DIAGRAM DESIGNATOR | 1 Y-ROTOR, 1 STATOR |