NSN 5990-00-469-4847
Part Details | TRANSMITTER SYNCHRO
5990-00-469-4847 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: 8175W12P006, 8175W12P002, CM41014105, CM41014126, 8175W12P002, HGC8SN9L887, HGC-8-SN9/L887, 5990-00-469-4847, 00-469-4847, 5990004694847, 004694847
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | MAR 03, 1972 | 00-469-4847 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-469-4847
Part Number | Cage Code | Manufacturer |
---|---|---|
8175W12P006 | 97424 | AMETEK INC.DBA AMETEK AEROSPACE & DEFENSE |
8175W12P002 | 97424 | AMETEK INC.DBA AMETEK AEROSPACE & DEFENSE |
CM41014105 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
CM41014126 | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
8175W12P002 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
HGC-8-SN9/L887 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-469-4847
Characteristic | Specifications |
---|---|
BODY SIZE | 8 |
ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
ROTOR INPUT CURRENT RATING | 26.1 MILLIAMPERES MINIMUM AND 31.9 MILLIAMPERES MAXIMUM |
ROTOR INPUT ELECTRICAL POWER RATING | 0.8 WATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ZRO RESISTANCE IN OHMS | 743.00 MINIMUM AND 1093.00 MAXIMUM |
PLUS J ZRO REACTANCE IN OHMS | 3465.00 MINIMUM AND 4245.00 MAXIMUM |
ZSO RESISTANCE IN OHMS | 7.62 MINIMUM AND 11.62 MAXIMUM |
PLUS J ZSO REACTANCE IN OHMS | 28.60 MINIMUM AND 41.40 MAXIMUM |
ZRS RESISTANCE IN OHMS | 1258.00 MINIMUM AND 1784.00 MAXIMUM |
PLUS J ZRS REACTANCE IN OHMS | 276.00 MINIMUM AND 484.00 MAXIMUM |
ROTOR DC RESISTANCE IN OHMS | 618.00 MINIMUM AND 770.00 MAXIMUM |
STATOR DC RESISTANCE IN OHMS | 8.80 MINIMUM AND 11.50 MAXIMUM |
TRANSFORMATION RATIO | 0.0995 ROTOR TO STATOR MINIMUM AND 0.1057 ROTOR TO STATOR MAXIMUM |
PHASE SHIFT ANGLE IN DEG | 13.200 INPUT TO OUTPUT MAXIMUM |
MAXIMUM TEMP RISE | 100.0 DEG CELSIUS |
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 75.00 OUTPUT |
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 75.00 |
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M14.0/P14.0 |
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.0 CENTIMETER-GRAMS NOMINAL |
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS NOMINAL |
BODY STYLE | STANDARD ROUND A |
PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
OVERALL LENGTH | 1.7880 INCHES MINIMUM AND 1.8180 INCHES MAXIMUM |
FLANGE DIAMETER | 0.7470 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
UNDERCUT DIAMETER | 0.6880 INCHES MINIMUM AND 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, STAINLESS |