NSN 5990-00-068-3592
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-068-3592 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: 68D40024, AY975B1, AY975B1, 5990-00-068-3592, 00-068-3592, 5990000683592, 000683592
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-068-3592 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-068-3592
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 68D40024 | 97151 | AIR FORCE LIFECYCLE MANAGEMENTCENTER ELECTRONIC COMPONENTS |
| AY975B1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY975B1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-068-3592
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 12 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 10.2 NOMINAL |
| STATOR INPUT CURRENT RATING | 86.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 170.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO IMPEDANCE MAGNITUDE IN OHMS | 777.50 NOMINAL |
| ZRO IMPEDANCE ANGLE IN DEG | 77.80 NOMINAL |
| ZSO IMPEDANCE MAGNITUDE IN OHMS | 132.50 NOMINAL |
| ZSO IMPEDANCE ANGLE IN DEG | 78.85 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 95.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 14.00 NOMINAL |
| TRANSFORMATION RATIO | 2.206 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 5.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 30.0 DEG CELSIUS |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 28.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M10.0/P10.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 55.00 INCH-OUNCES NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 11.00 INCH-OUNCES NOMINAL |
| BODY STYLE | 2 STANDARD ROUND A |
| SHOULDER DIAMETER | 1.0000 INCHES NOMINAL |
| PILOT DIAMETER | 0.6250 INCHES NOMINAL |
| OVERALL LENGTH | 2.8450 INCHES NOMINAL |
| FLANGE DIAMETER | 1.1880 INCHES NOMINAL |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 1.0000 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
| PILOT LENGTH | 0.0620 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 2.2670 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| SHAFT END PLAY | 0.0005 INCHES NOMINAL |
| SHAFT END PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0008 INCHES |