NSN 5990-00-677-6483
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-677-6483 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: 10511576, 5M621122001, 5M6211-220-01, AY1800A11K2, 18CT6B, 18CT6B, MILS2070834, MILS20708-34, 18CT6B, 4186800017, 4186800-017, 5990-00-677-6483, 00-677-6483, 5990006776483, 006776483
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-677-6483 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
Cross Reference | NSN 5990-00-677-6483
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 10511576 | 19204 | ARMY, UNITED STATES DEPARTMENT OFTHE |
| 5M6211-220-01 | D1901 | HENSOLDT SENSORS GMBHDIV SEPS |
| AY1800A11K2 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 18CT6B | C1834 | KONTRON AG |
| 18CT6B | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MILS20708-34 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 18CT6B | 95542 | NORTHROP GRUMMAN SYSTEMS CORPORATION |
| 4186800-017 | 05869 | RAYTHEON COMPANYDBA RAYTHEON |
Technical Data | NSN 5990-00-677-6483
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 18 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 20.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 360.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 60.0 NOMINAL |
| ZSO IMPEDANCE MAGNITUDE IN OHMS | 4600.00 MINIMUM AND 5800.00 MAXIMUM |
| ZSO IMPEDANCE ANGLE IN DEG | 70.00 MINIMUM AND 76.00 MAXIMUM |
| ZRS IMPEDANCE MAGNITUDE IN OHMS | 1600.00 MINIMUM AND 2050.00 MAXIMUM |
| ZRS IMPEDANCE ANGLE IN DEG | 14.50 MINIMUM AND 18.00 MAXIMUM |
| TRANSFORMATION RATIO | 0.735 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 16.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 10.0 DEG CELSIUS |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M6.0/P6.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 0.1 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND B |
| SHOULDER DIAMETER | 1.5625 INCHES NOMINAL |
| PILOT DIAMETER | 0.9370 INCHES NOMINAL |
| OVERALL LENGTH | 3.0600 INCHES NOMINAL |
| FLANGE DIAMETER | 1.7500 INCHES NOMINAL |
| FLANGE THICKNESS | 0.0937 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0785 INCHES NOMINAL |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| SHOULDER LENGTH | 0.1325 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 2.3880 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 1.0750 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |