NSN 5990-00-578-8842
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-578-8842 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: 11CT101A1, RS9011A, RS901-1A, 5RS9011A, 5RS901-1A, 5RS9011A, 5RS901-1A, 68400090101, TTC11E6, 546511, 54651-1, 8083414, 5990-00-578-8842, 00-578-8842, 5990005788842, 005788842
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-578-8842 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-578-8842
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 11CT101A1 | 06989 | API HAROWE INCDBA API MOTION DIV API |
| RS901-1A | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| 5RS901-1A | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| 5RS901-1A | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
| 68400090101 | 89944 | KOLLSMAN, INC. |
| TTC11E6 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 54651-1 | 96214 | RAYTHEON COMPANYDBA RAYTHEON |
| 8083414 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 5990-00-578-8842
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 165.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 250.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO IMPEDANCE MAGNITUDE IN OHMS | 74.30 NOMINAL |
| ZRO IMPEDANCE ANGLE IN DEG | 79.70 NOMINAL |
| ZSO IMPEDANCE MAGNITUDE IN OHMS | 418.00 NOMINAL |
| ZSO IMPEDANCE ANGLE IN DEG | 78.30 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 54.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 10.50 NOMINAL |
| TRANSFORMATION RATIO | 2.203 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 6.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 34.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 53.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M5.0/P5.0 |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 2.1600 INCHES MINIMUM AND 2.1840 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.0570 INCHES MINIMUM AND 1.0650 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.9750 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
| PILOT LENGTH | 0.0620 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.7960 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| FRAGILITY FACTOR | MODERATELY RUGGED |