NSN 5990-01-043-3400
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-01-043-3400 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: B8CT100H1, B8CT-100-H-1, 887C054025, 054025, HTC8A8L915, HTC-8-A-8/L915, HCT8A8L915, HCT-8-A-8/L915, 887C054025, 5990-01-043-3400, 01-043-3400, 5990010433400, 010433400
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JUN 23, 1977 | 01-043-3400 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
1 Y-ROTOR, 1 STATOR
Cross Reference | NSN 5990-01-043-3400
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| B8CT-100-H-1 | 06989 | API HAROWE INCDBA API MOTION DIV API |
| 887C054025 | 34228 | L3 TECHNOLOGIES, INC.DBA L3 KEO |
| 054025 | 34228 | L3 TECHNOLOGIES, INC.DBA L3 KEO |
| HTC-8-A-8/L915 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| HCT-8-A-8/L915 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 887C054025 | 03956 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS |
Technical Data | NSN 5990-01-043-3400
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 90.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 28.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 750.0 MILLIWATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 810.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 2700.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 470.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 1770.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 365.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 742.00 NOMINAL |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 100.00 INPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 125.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M10.0/P10.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 5.0 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 14.0 CENTIMETER-GRAMS MAXIMUM |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.6560 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.6910 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0430 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| SHAFT MAXIMUM RADIAL PLAY | 0.0005 INCHES |
| SHAFT RADIAL PLAY TEST POINT | 0.125 INCHES MAXIMUM |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT END PLAY | 0.0003 INCHES MINIMUM AND 0.0008 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 8.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| SCHEMATIC DIAGRAM DESIGNATOR | 1 Y-ROTOR, 1 STATOR |
| FRAGILITY FACTOR | MODERATELY RUGGED |
| END ITEM IDENTIFICATION | 2040-01-032-9085 |
