Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-244-8442 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: 101223, 10122-3, CM41004151, CM41004151, CTH8SW6A004, CTH8BE6A004, 5990-00-244-8442, 00-244-8442, 5990002448442, 002448442
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | FEB 12, 1969 | 00-244-8442 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-244-8442
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 10122-3 | 10138 | ASTRONAUTICS CORPORATION OF AMERICA |
| CM41004151 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| CM41004151 | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
| CTH8SW6A004 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CTH8BE6A004 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-244-8442
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 22.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 58.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 800.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 2500.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 120.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 450.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 440.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 280.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 550.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 100.00 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 9.200 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 12.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.0 CENTIMETER-GRAMS MAXIMUM |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.4710 INCHES NOMINAL |
| FLANGE DIAMETER | 0.7500 INCHES NOMINAL |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.6870 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0430 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| FRAGILITY FACTOR | MODERATELY RUGGED |