NSN 5990-00-683-0979
Part Details | TRANSMITTER SYNCHRO
5990-00-683-0979 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: CGH8RA8L212, 9001414, 900141-4, 5990-00-683-0979, 00-683-0979, 5990006830979, 006830979
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | JAN 01, 1963 | 00-683-0979 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
1 Y-ROTOR, 1 STATOR
Cross Reference | NSN 5990-00-683-0979
Part Number | Cage Code | Manufacturer |
---|---|---|
CGH8RA8L212 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
900141-4 | 06481 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS |
Technical Data | NSN 5990-00-683-0979
Characteristic | Specifications |
---|---|
BODY SIZE | 8 |
ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
ROTOR INPUT CURRENT RATING | 43.0 MILLIAMPERES MAXIMUM |
ROTOR INPUT ELECTRICAL POWER RATING | 1.5 WATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ZRO RESISTANCE IN OHMS | 933.00 NOMINAL |
PLUS J ZRO REACTANCE IN OHMS | 2985.00 NOMINAL |
ZSO RESISTANCE IN OHMS | 651.00 NOMINAL |
PLUS J ZSO REACTANCE IN OHMS | 1545.00 NOMINAL |
ROTOR DC RESISTANCE IN OHMS | 700.00 NOMINAL |
TRANSFORMATION RATIO | 0.783 ROTOR TO STATOR NOMINAL |
PHASE SHIFT ANGLE IN DEG | 17.000 INPUT TO OUTPUT MAXIMUM |
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 75.00 |
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 14.0 CENTIMETER-GRAMS MAXIMUM |
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 5.0 CENTIMETER-GRAMS MAXIMUM |
BODY STYLE | STANDARD ROUND A |
PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
OVERALL LENGTH | 1.6360 INCHES MAXIMUM |
FLANGE DIAMETER | 0.7490 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
UNDERCUT DIAMETER | 0.6910 INCHES MAXIMUM |
UNDERCUT WIDTH | 0.0570 INCHES MINIMUM |
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 END PLAY | 0.0001 INCHES MAXIMUM |
SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
SCHEMATIC DIAGRAM DESIGNATOR | 1 Y-ROTOR, 1 STATOR |
FRAGILITY FACTOR | MODERATELY RUGGED |