Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-090-3461 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: 508312S9L, 508-312S9L, 99924SCEE1011, 99924SCEE101-1, 5990-00-090-3461, 00-090-3461, 5990000903461, 000903461
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | NOV 29, 1972 | 00-090-3461 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-090-3461
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 508-312S9L | 99473 | HAWKER PACIFIC AEROSPACELANDING GEAR AND COMPONENTS MFG AND |
| 99924SCEE101-1 | 26512 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV MISSION SYSTEMS |
Technical Data | NSN 5990-00-090-3461
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 35.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 85.0 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 |
| ZRS RESISTANCE IN OHMS | 11.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 2.00 NOMINAL |
| ZRS IMPEDANCE MAGNITUDE IN OHMS | 830.00 MINIMUM AND 940.00 MAXIMUM |
| ZRS IMPEDANCE ANGLE IN DEG | 16.00 MINIMUM AND 20.00 MAXIMUM |
| 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 | 10.000 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 | 6.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.5000 INCHES NOMINAL |
| OVERALL LENGTH | 1.4050 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.7500 INCHES NOMINAL |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.7470 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0430 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.0150 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |