NSN 5990-00-882-8950
Part Details | TRANSMITTER SYNCHRO
5990-00-882-8950 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: 10068351, 10068351, 5990-00-882-8950, 00-882-8950, 5990008828950, 008828950
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1962 | 00-882-8950 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND D
Cross Reference | NSN 5990-00-882-8950
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 10068351 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
| 10068351 | 19200 | US ARMY ARDEC RDECOM |
Technical Data | NSN 5990-00-882-8950
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 23 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 264.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 3.0 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO IMPEDANCE MAGNITUDE IN OHMS | 470.00 MINIMUM AND 580.00 MAXIMUM |
| ZRO IMPEDANCE ANGLE IN DEG | 84.00 MINIMUM AND 87.50 MAXIMUM |
| ZSS IMPEDANCE MAGNITUDE IN OHMS | 21.60 MINIMUM AND 26.00 MAXIMUM |
| ZSS IMPEDANCE ANGLE IN DEG | 42.00 MINIMUM AND 47.00 MAXIMUM |
| TRANSFORMATION RATIO | 0.783 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 1.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 32.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 48.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M3.0/P3.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 0.2 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND D |
| SHOULDER DIAMETER | 1.9850 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM |
| PILOT DIAMETER | 0.5900 INCHES MINIMUM AND 0.6000 INCHES MAXIMUM |
| SECOND SHOULDER DIAMETER | 1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM |
| SECOND SHOULDER LENGTH | 0.2480 INCHES MINIMUM AND 0.2500 INCHES MAXIMUM |
| OVERALL LENGTH | 4.2990 INCHES MAXIMUM |
| FLANGE DIAMETER | 2.2490 INCHES MINIMUM AND 2.2500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.2030 INCHES NOMINAL |
| BODY DIAMETER | 1.9850 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM |
| PILOT LENGTH | 0.4050 INCHES MINIMUM AND 0.4220 INCHES MAXIMUM |
| SHOULDER LENGTH | 0.1570 INCHES MINIMUM AND 0.1720 INCHES MAXIMUM |
| AFT OF FIRST FLANGE DIAMETER | 1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 3.5800 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |
| FRAGILITY FACTOR | MODERATELY RUGGED |
