NSN 5990-00-929-8921
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-929-8921 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: 1497021, 35630800260, 3563080-0260, 35630800260, 3563080-0260, 35630800260, 3563080-0260, 1497021, 5990-00-929-8921, 00-929-8921, 5990009298921, 009298921
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | SEP 14, 1966 | 00-929-8921 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-929-8921
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1497021 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 3563080-0260 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 3563080-0260 | 02987 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX FLIGHT SYSTEMS |
| 3563080-0260 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 1497021 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-929-8921
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 40.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 70.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 425.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 1780.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 65.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 328.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 553.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 157.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 325.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 62.00 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 8.000 INPUT TO OUTPUT NOMINAL |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M20.0/P20.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.5000 INCHES NOMINAL |
| OVERALL LENGTH | 1.6250 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.7500 INCHES NOMINAL |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.6900 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2400 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| FRAGILITY FACTOR | MODERATELY RUGGED |
