Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-814-2239 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: 7R901022, 7R901-022, HTC11F8B889S, HTC-11-F-8/B889S, HTC11F8B889, HTC-11-F-8/B889, TTC11F8, U207322, 10043580, 5990-00-814-2239, 00-814-2239, 5990008142239, 008142239
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1962 | 00-814-2239 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-814-2239
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 7R901-022 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| HTC-11-F-8/B889S | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| HTC-11-F-8/B889 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| TTC11F8 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| U207322 | 82686 | TRANSICOIL LLCDBA ADS/TRANSICOIL |
| 10043580 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 5990-00-814-2239
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 90.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 17.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 250.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 707.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 3194.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 876.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 4580.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 637.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 324.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 370.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 602.00 NOMINAL |
| TRANSFORMATION RATIO | 0.735 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 3.400 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 1.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 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 | 2.3580 INCHES NOMINAL |
| FLANGE DIAMETER | 1.0590 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.9700 INCHES MINIMUM AND 0.9750 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
| PILOT LENGTH | 0.0620 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.7950 INCHES MAXIMUM |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES MAXIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8120 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |