NSN 5990-00-779-6844
Part Details | TRANSMITTER SYNCHRO
5990-00-779-6844 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: M010951, M01095-1, AY201S77T, AY201S-77-T, 706560, AY201S77T, AY201S-77-T, 706560, CGH15DS1A004, CGH-15-DS-1A004, CGH15D11A004, CGH-15-D-11/A004, 4068631, 406863-1, 5990-00-779-6844, 00-779-6844, 5990007796844, 007796844
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1962 | 00-779-6844 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
1 Y-ROTOR, 1 STATOR
Cross Reference | NSN 5990-00-779-6844
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| M01095-1 | 80249 | BAE SYSTEMS INFORMATION ANDELECTRONIC SYSTEMS INTEGRATION INC. |
| AY201S-77-T | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 706560 | 07187 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY201S-77-T | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 706560 | 56232 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| CGH-15-DS-1A004 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CGH-15-D-11/A004 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 406863-1 | 96214 | RAYTHEON COMPANYDBA RAYTHEON |
Technical Data | NSN 5990-00-779-6844
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 226.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 1.25 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 19.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 112.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 4.70 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 19.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 21.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 13.00 NOMINAL |
| ZSO-90 RESISTANCE IN OHMS | 3.30 NOMINAL |
| PLUS J ZSO-90 REACTANCE IN OHMS | 5.70 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 8.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 3.60 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 3.900 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M10.0/P10.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 30.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 10.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 1.3120 INCHES MAXIMUM |
| PILOT DIAMETER | 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 2.1930 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.4370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0980 INCHES MAXIMUM |
| UNDERCUT DIAMETER | 1.3150 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0880 INCHES MAXIMUM |
| PILOT LENGTH | 0.0450 INCHES MAXIMUM |
| SHOULDER LENGTH | 0.1370 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6620 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |
| SHAFT MAXIMUM RADIAL PLAY | 0.0010 INCHES |
| SHAFT RADIAL PLAY TEST POINT | 0.125 INCHES MAXIMUM |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT END PLAY | 0.0003 INCHES MINIMUM AND 0.0015 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| SCHEMATIC DIAGRAM DESIGNATOR | 1 Y-ROTOR, 1 STATOR |
| FRAGILITY FACTOR | MODERATELY RUGGED |
