NSN 5990-00-458-9643
Part Details | TRANSMITTER SYNCHRO
5990-00-458-9643 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: 12470183, 1247018-3, 35633100003, 3563310-0003, 12470183, 1247018-3, 35633100003, 3563310-0003, 31TX6XN1, 1590096, 5990-00-458-9643, 00-458-9643, 5990004589643, 004589643
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 02, 1970 | 00-458-9643 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND D
Cross Reference | NSN 5990-00-458-9643
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1247018-3 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 3563310-0003 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 1247018-3 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 3563310-0003 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 31TX6XN1 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 1590096 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
Technical Data | NSN 5990-00-458-9643
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 32 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 420.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 5.5 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| TRANSFORMATION RATIO | 0.783 ROTOR TO STATOR NOMINAL |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 20.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 75.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M10.0/P10.0 |
| TORQUE GRADIENT PER ANGULAR DEG | 0.400 INCH-OUNCES MINIMUM |
| BODY STYLE | STANDARD ROUND D |
| SHOULDER DIAMETER | 2.6950 INCHES MINIMUM AND 2.7000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.2900 INCHES NOMINAL |
| SECOND SHOULDER DIAMETER | 2.7500 INCHES NOMINAL |
| SECOND SHOULDER LENGTH | 0.3750 INCHES NOMINAL |
| OVERALL LENGTH | 5.1000 INCHES NOMINAL |
| FLANGE DIAMETER | 3.0980 INCHES MINIMUM AND 3.1000 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.2500 INCHES NOMINAL |
| BODY DIAMETER | 2.7000 INCHES MAXIMUM |
| PILOT LENGTH | 0.0300 INCHES NOMINAL |
| SHOULDER LENGTH | 0.6150 INCHES NOMINAL |
| AFT OF FIRST FLANGE DIAMETER | 2.7500 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 4.3700 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |