Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-813-1820 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: VCT23366B, VCT23/36-6B, AY240BA 10 A1, MILS2070894, MIL-S20708/94, 23CT6A, MS510804, MS51080-4, 23CT6A, 3151127P6, 315-1127P6, 5990-00-813-1820, 00-813-1820, 5990008131820, 008131820
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-813-1820 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5990-00-813-1820
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| VCT23/36-6B | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| AY240BA 10 A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| MIL-S20708/94 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 23CT6A | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MS51080-4 | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
| 23CT6A | 95542 | NORTHROP GRUMMAN SYSTEMS CORPORATION |
| 315-1127P6 | 99687 | RAYTHEON CO EQUIPMENT DEVELOPMENTLAB |
Technical Data | NSN 5990-00-813-1820
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 23 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 90.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 22.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 600.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 60.0 NOMINAL |
| TRANSFORMATION RATIO | 0.735 ROTOR TO STATOR NOMINAL |
| OVERALL LENGTH | 3.5800 INCHES NOMINAL |
| FLANGE DIAMETER | 2.2500 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 7 SCREW |
| BODY MATERIAL | ANY ACCEPTABLE |
| FRAGILITY FACTOR | MODERATELY RUGGED |