NSN 5990-00-359-9813
Part Details | TRANSMITTER SYNCHRO
5990-00-359-9813 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: 5472830P20, EGH8A7A013, 5990-00-359-9813, 00-359-9813, 5990003599813, 003599813
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | FEB 18, 1974 | 00-359-9813 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-359-9813
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5472830P20 | 97424 | AMETEK INC.DBA AMETEK AEROSPACE & DEFENSE |
| EGH8A7A013 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-359-9813
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 100.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 540.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 45.90 MINIMUM AND 62.10 MAXIMUM |
| PLUS J ZRO REACTANCE IN OHMS | 234.00 MINIMUM AND 286.00 MAXIMUM |
| ZSO RESISTANCE IN OHMS | 10.20 MINIMUM AND 13.80 MAXIMUM |
| PLUS J ZSO REACTANCE IN OHMS | 540.50 NOMINAL |
| ZRS RESISTANCE IN OHMS | 66.80 MINIMUM AND 93.20 MAXIMUM |
| PLUS J ZRS REACTANCE IN OHMS | 17.80 MINIMUM AND 22.20 MAXIMUM |
| ROTOR DC RESISTANCE IN OHMS | 33.30 MINIMUM AND 40.70 MAXIMUM |
| STATOR DC RESISTANCE IN OHMS | 10.80 MINIMUM AND 13.20 MAXIMUM |
| PHASE SHIFT ANGLE IN DEG | 8.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 30.00 OUTPUT |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 6.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS NOMINAL |
| TORQUE GRADIENT PER ANGULAR DEG | 2200.0 MILLIMETER-MILLIGRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.9380 INCHES NOMINAL |
| FLANGE DIAMETER | 0.7490 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 | 1.3680 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 TURRET |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ANY ACCEPTABLE |
| FRAGILITY FACTOR | MODERATELY RUGGED |