Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-119-5699 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: CM91004038, CM91004038, 123SCPE53241, 123SCPE5324-1, 5990-00-119-5699, 00-119-5699, 5990001195699, 001195699
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 04, 1973 | 00-119-5699 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-119-5699
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CM91004038 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| CM91004038 | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
| 123SCPE5324-1 | 26512 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV MISSION SYSTEMS |
Technical Data | NSN 5990-00-119-5699
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 30.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 73.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 470.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 1770.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 81.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 330.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 365.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 64.00 NOMINAL |
| TRANSFORMATION RATIO | 2.203 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 8.200 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 12.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 25.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M5.0/P5.0 |
| 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 A |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 2.1400 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.7470 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| UNDERCUT DIAMETER | 0.6880 INCHES MINIMUM AND 0.6910 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| PILOT LENGTH | 0.0370 INCHES MINIMUM AND 0.0430 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.3680 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 TURRET |
| TERMINAL LOCATION | REAR |
| FRAGILITY FACTOR | MODERATELY RUGGED |