NSN 5990-01-223-9414
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-01-223-9414 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: 8CT480D17G, 8CT-480-D-17G, 144A8700P2, 144A8700P2, 144A8700P2, 08GJT21LFJO60, 08-GJT-21LF/JO60, 5990-01-223-9414, 01-223-9414, 5990012239414, 012239414
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 10, 1986 | 01-223-9414 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-01-223-9414
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 8CT-480-D-17G | 06989 | API HAROWE INCDBA API MOTION DIV API |
| 144A8700P2 | 89954 | BAE SYSTEMS CONTROLS INC. |
| 144A8700P2 | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
| 144A8700P2 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 08-GJT-21LF/JO60 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-01-223-9414
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 23.0 MILLIAMPERES MAXIMUM |
| STATOR INPUT ELECTRICAL POWER RATING | 41.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 640.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 2800.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 110.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 510.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 830.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 310.00 NOMINAL |
| ZSS RESISTANCE IN OHMS | 150.00 NOMINAL |
| PLUS J ZSS REACTANCE IN OHMS | 60.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 480.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 105.00 NOMINAL |
| TRANSFORMATION RATIO | 2.203 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 8.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 0.20 INCH-OUNCES MAXIMUM |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.5920 INCHES NOMINAL |
| FLANGE DIAMETER | 0.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.6870 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2400 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |
| FRAGILITY FACTOR | MODERATELY RUGGED |
