NSN 5990-00-922-2449
Part Details | TRANSMITTER SYNCHRO
5990-00-922-2449 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: 10181799, 10181799, 000011474, 000-011474, 10181799, 11CX4E2002, 11CX4E/2-002, 10181799, 11CX9222449, 11CX922-2449, U219604, U-219604, 10181799, 10181799, 5990-00-922-2449, 00-922-2449, 5990009222449, 009222449
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | APR 24, 1968 | 00-922-2449 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
Cross Reference | NSN 5990-00-922-2449
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 10181799 | 14404 | AMETEK TECHNICAL & INDUSTRIALPRODUCTS, INC. |
| 10181799 | 51761 | CDA INTERCORP LLC |
| 000-011474 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| 10181799 | 1K426 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 11CX4E/2-002 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 10181799 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 11CX922-2449 | 2X130 | MOTION DEVICES TECHNOLOGY, INC. |
| U-219604 | 82686 | TRANSICOIL LLCDBA ADS/TRANSICOIL |
| 10181799 | 82686 | TRANSICOIL LLCDBA ADS/TRANSICOIL |
| 10181799 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 5990-00-922-2449
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 114.0 MINIMUM AND 116.0 MAXIMUM |
| ROTOR INPUT CURRENT RATING | 31.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 490.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 396.0 MINIMUM AND 404.0 MAXIMUM |
| ZRO IMPEDANCE MAGNITUDE IN OHMS | 3720.00 MINIMUM AND 4700.00 MAXIMUM |
| ZRO IMPEDANCE ANGLE IN DEG | 80.00 MINIMUM AND 84.00 MAXIMUM |
| ZSS IMPEDANCE MAGNITUDE IN OHMS | 410.00 MINIMUM AND 500.00 MAXIMUM |
| ZSS IMPEDANCE ANGLE IN DEG | 17.00 MINIMUM AND 26.00 MAXIMUM |
| TRANSFORMATION RATIO | 0.783 STATOR TO ROTOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 3.000 INPUT TO OUTPUT MINIMUM AND 6.000 INPUT TO OUTPUT MAXIMUM |
| MAXIMUM TEMP RISE | 20.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 45.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 75.00 |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 0.07 INCH-OUNCES NOMINAL |
| BODY STYLE | STANDARD ROUND B |
| SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 2.3560 INCHES NOMINAL |
| FLANGE DIAMETER | 1.0570 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 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 | 1.7320 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8090 INCHES MINIMUM AND 0.8150 INCHES MAXIMUM |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ANY ACCEPTABLE |
| TEST DATA DOCUMENT | 18876-10181799 DRAWING (THIS IS THE BASIC GOVERNING DRAWING, SUCH AS A CONTRACTOR DRAWING, ORIGINAL EQUIPMENT MANUFACTURER DRAWING, ETC.; EXCLUDES ANY SPECIFICATION, STANDARD OR OTHER DOCUMENT THAT MAY BE REFERENCED IN A BASIC GOVERNING DRAWING) |
| FRAGILITY FACTOR | MODERATELY RUGGED |
