NSN 5990-00-465-4903
Part Details | TRANSMITTER SYNCHRO
5990-00-465-4903 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: AY100EC105A1, 1497629, AY100EC105A1, 1497629, 5990-00-465-4903, 00-465-4903, 5990004654903, 004654903
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | JAN 19, 1970 | 00-465-4903 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-465-4903
Part Number | Cage Code | Manufacturer |
---|---|---|
AY100EC105A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
1497629 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
AY100EC105A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
1497629 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-465-4903
Characteristic | Specifications |
---|---|
BODY SIZE | 10 |
ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
ROTOR INPUT CURRENT RATING | 40.0 MILLIAMPERES MAXIMUM |
ROTOR INPUT ELECTRICAL POWER RATING | 800.0 MILLIWATTS MAXIMUM |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ZRO RESISTANCE IN OHMS | 563.00 NOMINAL |
PLUS J ZRO REACTANCE IN OHMS | 3080.00 NOMINAL |
ZSO RESISTANCE IN OHMS | 6.25 NOMINAL |
PLUS J ZSO REACTANCE IN OHMS | 24.80 NOMINAL |
ZRS RESISTANCE IN OHMS | 821.00 NOMINAL |
PLUS J ZRS REACTANCE IN OHMS | 314.00 NOMINAL |
ROTOR DC RESISTANCE IN OHMS | 321.00 NOMINAL |
STATOR DC RESISTANCE IN OHMS | 5.85 NOMINAL |
TRANSFORMATION RATIO | 0.103 ROTOR TO STATOR NOMINAL |
PHASE SHIFT ANGLE IN DEG | 8.000 INPUT TO OUTPUT NOMINAL |
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 50.00 |
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M15.0/P15.0 |
TORQUE GRADIENT PER ANGULAR DEG | 2900.0 MILLIMETER-MILLIGRAMS MAXIMUM |
BODY STYLE | STANDARD ROUND C |
SHOULDER DIAMETER | 0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM |
PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
OVERALL LENGTH | 1.4130 INCHES MAXIMUM |
FLANGE DIAMETER | 0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM |
FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
UNDERCUT DIAMETER | 0.8350 INCHES MINIMUM AND 0.8400 INCHES MAXIMUM |
UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
PILOT LENGTH | 0.0380 INCHES NOMINAL |
SHOULDER LENGTH | 0.0630 INCHES NOMINAL |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2650 INCHES MAXIMUM |
ALIGNMENT HOLE DEPTH | 0.0730 INCHES MINIMUM |
ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.6750 INCHES MINIMUM AND 0.6810 INCHES MAXIMUM |
ALIGNMENT HOLE QUANTITY | 3 |
TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
TERMINAL LOCATION | SIDE |
BODY MATERIAL | STEEL, STAINLESS |