NSN 5990-00-033-5155
Part Details | DIFFERENTIAL TRANSMITTER SYNCHRO
5990-00-033-5155 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: M01026E, AY231S25, AY231S25, AY23153, AY231S3, CP35991L, CP35-9-9-1L, 15403903, 15-4039-03, 1JD2136P11, 1JD2136PT11, 1JD213611, 1JD2136-11, 1JD213611, 1JD2136-11, 5990-00-033-5155, 00-033-5155, 5990000335155, 000335155
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-033-5155 | 02071 ( SYNCHRO, DIFFERENTIAL TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
Cross Reference | NSN 5990-00-033-5155
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| M01026E | 80249 | BAE SYSTEMS INFORMATION ANDELECTRONIC SYSTEMS INTEGRATION INC. |
| AY231S25 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY231S25 | 19315 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND |
| AY23153 | 19315 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND |
| AY231S3 | 19315 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND |
| CP35-9-9-1L | 25500 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| 15-4039-03 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 1JD2136P11 | 79500 | WESTINGHOUSE ELECTRIC CORP |
| 1JD2136PT11 | 79500 | WESTINGHOUSE ELECTRIC CORP |
| 1JD2136-11 | 79500 | WESTINGHOUSE ELECTRIC CORP |
| 1JD2136-11 | 65054 | WESTINGHOUSE ELECTRIC CORPPOWER GENERATION-GENERATOR DIV |
Technical Data | NSN 5990-00-033-5155
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 120.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 1.3 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 90.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 200.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 14.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 10.80 NOMINAL |
| TRANSFORMATION RATIO | 0.450 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 35.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 15.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M12.0/P12.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.00 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 7.00 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND B |
| SHOULDER DIAMETER | 1.3120 INCHES NOMINAL |
| PILOT DIAMETER | 0.5000 INCHES NOMINAL |
| OVERALL LENGTH | 2.1310 INCHES NOMINAL |
| FLANGE DIAMETER | 1.4370 INCHES NOMINAL |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0780 INCHES NOMINAL |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| SHOULDER LENGTH | 0.1320 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.4590 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8750 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 6 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |