Part Details | CONTROL TRANSFORMER SYNCHRO
5990-01-042-1984 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: 2692782, 15CT4, VCT154M2, VCT15-4M2, 2692782, 2692782, 5990-01-042-1984, 01-042-1984, 5990010421984, 010421984
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JUN 07, 1977 | 01-042-1984 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
Cross Reference | NSN 5990-01-042-1984
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2692782 | 44114 | BAE SYSTEMS LAND & ARMAMENTS L.P. |
| 15CT4 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| VCT15-4M2 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| 2692782 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| 2692782 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
Technical Data | NSN 5990-01-042-1984
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 1.31 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 2.4 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZSO IMPEDANCE MAGNITUDE IN OHMS | 7800.00 MINIMUM AND 9512.00 MAXIMUM |
| ZSO IMPEDANCE ANGLE IN DEG | 78.80 MINIMUM AND 84.50 MAXIMUM |
| ZRS IMPEDANCE MAGNITUDE IN OHMS | 1050.00 MINIMUM AND 1300.00 MAXIMUM |
| ZRS IMPEDANCE ANGLE IN DEG | 26.00 MINIMUM AND 33.00 MAXIMUM |
| PHASE SHIFT ANGLE IN DEG | 5.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 10.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 4.19 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 7.86 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M6.0/P6.0 |
| BODY STYLE | STANDARD ROUND B |
| SHOULDER DIAMETER | 1.3120 INCHES NOMINAL |
| PILOT DIAMETER | 0.8750 INCHES NOMINAL |
| OVERALL LENGTH | 2.3220 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.4370 INCHES NOMINAL |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0780 INCHES NOMINAL |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| SHOULDER LENGTH | 0.1320 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6400 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| FRAGILITY FACTOR | MODERATELY RUGGED |