Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-811-3275 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: AB973, CT11A25, CT-11-A-25, 9900001, 990000-1, 5990-00-811-3275, 00-811-3275, 5990008113275, 008113275
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) | 
|---|---|---|---|
| 59 | JAN 01, 1962 | 00-811-3275 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) | 
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
 
					Cross Reference | NSN 5990-00-811-3275
| Part Number | Cage Code | Manufacturer | 
|---|---|---|
| AB973 | 61349 | AMETEK, INC.DIV AEROSPACE & DEFENSE | 
| CT-11-A-25 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP | 
| 990000-1 | 82577 | RAYTHEON COMPANYDBA RAYTHEON | 
Technical Data | NSN 5990-00-811-3275
| Characteristic | Specifications | 
|---|---|
| BODY SIZE | 11 | 
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL | 
| STATOR INPUT CURRENT RATING | 161.0 MILLIAMPERES NOMINAL | 
| STATOR INPUT ELECTRICAL POWER RATING | 400.0 MILLIWATTS NOMINAL | 
| FREQUENCY IN HERTZ | 400.0 NOMINAL | 
| ZRO IMPEDANCE MAGNITUDE IN OHMS | 299.00 NOMINAL | 
| ZRO IMPEDANCE ANGLE IN DEG | 71.80 NOMINAL | 
| ZSO IMPEDANCE MAGNITUDE IN OHMS | 63.40 NOMINAL | 
| ZSO IMPEDANCE ANGLE IN DEG | 76.00 NOMINAL | 
| ROTOR DC RESISTANCE IN OHMS | 53.00 NOMINAL | 
| STATOR DC RESISTANCE IN OHMS | 11.00 NOMINAL | 
| PHASE SHIFT ANGLE IN DEG | 6.500 INPUT TO OUTPUT NOMINAL | 
| MAXIMUM TEMP RISE | 1.0 DEG CELSIUS | 
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 70.00 | 
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M10.0/P10.0 | 
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.0 CENTIMETER-GRAMS MAXIMUM | 
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.0 CENTIMETER-GRAMS MAXIMUM | 
| BODY STYLE | STANDARD ROUND C | 
| SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM | 
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM | 
| OVERALL LENGTH | 2.1830 INCHES NOMINAL | 
| FLANGE DIAMETER | 1.0620 INCHES NOMINAL | 
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL | 
| UNDERCUT DIAMETER | 0.9620 INCHES NOMINAL | 
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL | 
| PILOT LENGTH | 0.0620 INCHES NOMINAL | 
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL | 
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.8010 INCHES MAXIMUM | 
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD | 
| TERMINAL LOCATION | REAR | 
| BODY MATERIAL | STEEL, CORROSION RESISTING |