NSN 5990-00-725-7811
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-725-7811 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: CTH10JS12B337, CTH-10-JS-12/B337, CTC10JS12, CSDH10JS5, CSDH-10-JS-5, 2102297, 10032596, 5990-00-725-7811, 00-725-7811, 5990007257811, 007257811
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | JAN 01, 1963 | 00-725-7811 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
Cross Reference | NSN 5990-00-725-7811
Part Number | Cage Code | Manufacturer |
---|---|---|
CTH-10-JS-12/B337 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
CTC10JS12 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
CSDH-10-JS-5 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
2102297 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
10032596 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 5990-00-725-7811
Characteristic | Specifications |
---|---|
BODY SIZE | 10 |
STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
STATOR INPUT CURRENT RATING | 80.0 MILLIAMPERES NOMINAL |
STATOR INPUT ELECTRICAL POWER RATING | 190.0 MILLIWATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ZRO RESISTANCE IN OHMS | 80.00 NOMINAL |
PLUS J ZRO REACTANCE IN OHMS | 180.00 NOMINAL |
ZSO RESISTANCE IN OHMS | 29.00 NOMINAL |
PLUS J ZSO REACTANCE IN OHMS | 124.00 NOMINAL |
ROTOR DC RESISTANCE IN OHMS | 70.00 NOMINAL |
STATOR DC RESISTANCE IN OHMS | 25.00 NOMINAL |
PHASE SHIFT ANGLE IN DEG | 8.500 INPUT TO OUTPUT NOMINAL |
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 30.00 INPUT |
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M15.0/P15.0 |
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 B |
SHOULDER DIAMETER | 0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM |
PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
OVERALL LENGTH | 1.8430 INCHES MAXIMUM |
FLANGE DIAMETER | 0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM |
FLANGE THICKNESS | 0.0630 INCHES NOMINAL |
UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
PILOT LENGTH | 0.0380 INCHES NOMINAL |
SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.1810 INCHES NOMINAL |
TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
TERMINAL LOCATION | REAR |
BODY MATERIAL | ANY ACCEPTABLE |
SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |