NSN 5990-01-122-5629
Part Details | TRANSMITTER SYNCHRO
5990-01-122-5629 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the stator into a receiver synchro, a control transformer or differential synchro is dependent upon the position of its rotor. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: 35631505012, 3563150-5012, VCX1560296, VCX15-602-96, VCX156D296, VCX15-6D2-96, 35631505012, 3563150-5012, 35631505012, 3563150-5012, 1809976, 1802884150, 1802884-150, 5990-01-122-5629, 01-122-5629, 5990011225629, 011225629
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | NOV 25, 1981 | 01-122-5629 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
Cross Reference | NSN 5990-01-122-5629
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3563150-5012 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| VCX15-602-96 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| VCX15-6D2-96 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| 3563150-5012 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 3563150-5012 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 1809976 | 03956 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS |
| 1802884-150 | 03956 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS |
Technical Data | NSN 5990-01-122-5629
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 22.0 AMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 360.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 60.0 NOMINAL |
| ZRO IMPEDANCE MAGNITUDE IN OHMS | 5780.00 NOMINAL |
| ZRO IMPEDANCE ANGLE IN DEG | 78.00 MINIMUM AND 85.00 MAXIMUM |
| ZSS IMPEDANCE MAGNITUDE IN OHMS | 750.00 NOMINAL |
| ZSS IMPEDANCE ANGLE IN DEG | 11.00 MINIMUM AND 16.00 MAXIMUM |
| TRANSFORMATION RATIO | 0.783 STATOR TO ROTOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 7.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 20.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 20.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 120.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M6.0/P6.0 |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 0.05 INCH-OUNCES NOMINAL |
| BODY STYLE | STANDARD ROUND B |
| SHOULDER DIAMETER | 1.3120 INCHES NOMINAL |
| PILOT DIAMETER | 0.8750 INCHES NOMINAL |
| OVERALL LENGTH | 3.0630 INCHES NOMINAL |
| FLANGE DIAMETER | 1.4370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0780 INCHES NOMINAL |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| SHOULDER LENGTH | 0.1170 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 2.5080 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 1.1000 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 6 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| SHAFT MAXIMUM RADIAL PLAY | 0.0004 INCHES |
| SHAFT RADIAL PLAY TEST POINT | 0.430 INCHES NOMINAL |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 8.0 OUNCES |
| SHAFT END PLAY | 0.0015 INCHES NOMINAL |
| SHAFT END PLAY DETERMINING WEIGHT | 8.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0008 INCHES |
| FRAGILITY FACTOR | MODERATELY RUGGED |
