NSN 5990-00-779-4175
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-779-4175 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: 08CT11021, 08CT1102-1, 8CT300C110, 8CT-300-C-1/10, 101221REVA, 10122-1REVA, 101221, 10122-1, 08CT0134B, 08CT-0134-B, 43450021, 0083132, 008-313-2, R10012C, R1001-2C, CM41004084, CM1004084, 101221, 10122-1, CM41004084, 0083132, 008-313-2, CTH8A6A004, CTH8A6A004, CTH-8-A-6/A004, 101221, 10122-1, 5990-00-779-4175, 00-779-4175, 5990007794175, 007794175
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1960 | 00-779-4175 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-779-4175
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 08CT1102-1 | 14404 | AMETEK TECHNICAL & INDUSTRIALPRODUCTS, INC. |
| 8CT-300-C-1/10 | 06989 | API HAROWE INCDBA API MOTION DIV API |
| 10122-1REVA | 10138 | ASTRONAUTICS CORPORATION OF AMERICA |
| 10122-1 | 10138 | ASTRONAUTICS CORPORATION OF AMERICA |
| 08CT-0134-B | 51761 | CDA INTERCORP LLC |
| 43450021 | 03988 | HOHL MACHINE AND CONVEYOR CO INC |
| 008-313-2 | 99743 | IMC MAGNETICS CORPWESTERN DIV |
| R1001-2C | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| CM41004084 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| CM1004084 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| 10122-1 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| CM41004084 | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
| 008-313-2 | 92703 | KEMTRON ELECTRON PRODUCTS INC |
| CTH8A6A004 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CTH-8-A-6/A004 | 4H618 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 10122-1 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-779-4175
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 30.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 100.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| TRANSFORMATION RATIO | 1.900 ROTOR TO STATOR NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 12.0 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS MAXIMUM |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.6160 INCHES NOMINAL |
| FLANGE DIAMETER | 0.7500 INCHES NOMINAL |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.6870 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0430 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| FRAGILITY FACTOR | MODERATELY RUGGED |