NSN 5990-00-729-9624
Part Details | DIFFERENTIAL TRANSMITTER SYNCHRO
5990-00-729-9624 A synchro, the rotor of which is mechanically positioned for modifying electrical angular information, received from a transmitter synchro and transmitting to receiver synchro or control transformer synchro electrical information corresponding to the sum or difference of the electrical input angle and its rotor position angle. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: 23CDX1343, VCDX234N22, VCDX23/4N22, X14845141, X1484514-1, AY2435E3B2, AY2435E3B2, AV2435E3B2, X14845141, X1484514-1, 9174893, 5990-00-729-9624, 00-729-9624, 5990007299624, 007299624
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-729-9624 | 02071 ( SYNCHRO, DIFFERENTIAL TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND D
Cross Reference | NSN 5990-00-729-9624
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 23CDX1343 | 14404 | AMETEK TECHNICAL & INDUSTRIALPRODUCTS, INC. |
| VCDX23/4N22 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| X1484514-1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY2435E3B2 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY2435E3B2 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AV2435E3B2 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| X1484514-1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 9174893 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 5990-00-729-9624
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 23 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 90.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 230.0 MILLIAMPERES MINIMUM AND 297.0 MILLIAMPERES MAXIMUM |
| STATOR INPUT ELECTRICAL POWER RATING | 1.6 WATTS MINIMUM AND 2.4 WATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| TRANSFORMATION RATIO | 1.154 ROTOR TO STATOR NOMINAL |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 40.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 75.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
| BODY STYLE | STANDARD ROUND D |
| SHOULDER DIAMETER | 1.9900 INCHES MINIMUM AND 1.9940 INCHES MAXIMUM |
| PILOT DIAMETER | 0.5900 INCHES MINIMUM AND 0.6000 INCHES MAXIMUM |
| SECOND SHOULDER DIAMETER | 1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM |
| SECOND SHOULDER LENGTH | 0.1700 INCHES NOMINAL |
| OVERALL LENGTH | 5.3840 INCHES MINIMUM AND 5.4100 INCHES MAXIMUM |
| FLANGE DIAMETER | 2.2490 INCHES MINIMUM AND 2.2500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.2480 INCHES MINIMUM AND 0.2500 INCHES MAXIMUM |
| BODY DIAMETER | 1.9900 INCHES MAXIMUM |
| PILOT LENGTH | 0.0430 INCHES NOMINAL |
| SHOULDER LENGTH | 0.1700 INCHES NOMINAL |
| AFT OF FIRST FLANGE DIAMETER | 1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 3.4100 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 6 TAB W/SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| FRAGILITY FACTOR | MODERATELY RUGGED |