NSN 5990-00-623-4196
Part Details | TRANSMITTER SYNCHRO
5990-00-623-4196 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: RS9112E, RS911-2E, 9177568, RS9112E, RS911-2E, 9177568, TGH11F8A004, TGH-11-F-8/A004, TGH11F8A004, TGH-11-F-8/A004, TGC11F80, TGC-11-F80, TGC11F8A004, TGC-11-F-8/A004, 9177568, U216940, U-216940, 9177568, 9072628, 5990-00-623-4196, 00-623-4196, 5990006234196, 006234196
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-623-4196 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-623-4196
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| RS911-2E | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| 9177568 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| RS911-2E | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
| 9177568 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| TGH-11-F-8/A004 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| TGH-11-F-8/A004 | 4H618 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| TGC-11-F80 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| TGC-11-F-8/A004 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 9177568 | 49956 | RAYTHEON COMPANYDBA RAYTHEON |
| U-216940 | 82686 | TRANSICOIL LLCDBA ADS/TRANSICOIL |
| 9177568 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
| 9072628 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 5990-00-623-4196
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 60.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 800.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO IMPEDANCE MAGNITUDE IN OHMS | 2210.00 NOMINAL |
| ZRO IMPEDANCE ANGLE IN DEG | 82.30 NOMINAL |
| ZSO IMPEDANCE MAGNITUDE IN OHMS | 1130.00 NOMINAL |
| ZSO IMPEDANCE ANGLE IN DEG | 81.30 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 159.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 137.00 NOMINAL |
| TRANSFORMATION RATIO | 0.783 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 4.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 15.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 59.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 94.00 |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 2.3580 INCHES NOMINAL |
| FLANGE DIAMETER | 1.0570 INCHES MINIMUM AND 1.0650 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.9750 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
| PILOT LENGTH | 0.0620 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.7960 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |
| FRAGILITY FACTOR | MODERATELY RUGGED |