Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-725-7811 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: CTC10JS12, CSDH10JS5, CSDH-10-JS-5, CTH10JS12B337, CTH-10-JS-12/B337, 2102297, 10032596, 5990-00-725-7811, 00-725-7811, 5990007257811, 007257811
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-725-7811 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
Cross Reference | NSN 5990-00-725-7811
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CTC10JS12 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CSDH-10-JS-5 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CTH-10-JS-12/B337 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 2102297 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
| 10032596 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 5990-00-725-7811
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 80.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 190.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 80.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 180.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 29.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 124.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 70.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 25.00 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 8.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 30.00 INPUT |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M15.0/P15.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND B |
| SHOULDER DIAMETER | 0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.8430 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0630 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0380 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.1810 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ANY ACCEPTABLE |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |