NSN 5990-00-649-8352
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-649-8352 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: 23CT1382, VCT23484G, VCT23/48-4G, CT234G, CT23-4G, N21809, 9091809, 5990-00-649-8352, 00-649-8352, 5990006498352, 006498352
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-649-8352 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND D
Cross Reference | NSN 5990-00-649-8352
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 23CT1382 | 14404 | AMETEK TECHNICAL & INDUSTRIALPRODUCTS, INC. |
| VCT23/48-4G | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| CT23-4G | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| N21809 | 76823 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE |
| 9091809 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 5990-00-649-8352
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 23 |
| BODY STYLE | STANDARD ROUND D |
| SHOULDER DIAMETER | 1.9875 INCHES NOMINAL |
| PILOT DIAMETER | 0.6000 INCHES MAXIMUM |
| SECOND SHOULDER DIAMETER | 1.9990 INCHES NOMINAL |
| SECOND SHOULDER LENGTH | 0.4210 INCHES NOMINAL |
| OVERALL LENGTH | 5.7900 INCHES MAXIMUM |
| FLANGE DIAMETER | 2.2495 INCHES NOMINAL |
| FLANGE THICKNESS | 0.4175 INCHES NOMINAL |
| BODY DIAMETER | 1.9985 INCHES MAXIMUM |
| PILOT LENGTH | 0.0460 INCHES NOMINAL |
| SHOULDER LENGTH | 0.7060 INCHES NOMINAL |
| AFT OF FIRST FLANGE DIAMETER | 1.9990 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 1 CONNECTOR, PLUG |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| FRAGILITY FACTOR | MODERATELY RUGGED |