NSN 5990-00-754-8135
Part Details | TRANSMITTER SYNCHRO
5990-00-754-8135 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: 521003, 831713018, 8317-13018, 66334, 66-334, CGH10AS4, CGH-10-AS-4, CGC10AS4, 831713018, 8317-13018, 1180000002, 11-800-00-002, 4132651, 413265-1, 83173223, 8317-3223, 10515472, 5990-00-754-8135, 00-754-8135, 5990007548135, 007548135
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1962 | 00-754-8135 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-754-8135
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 521003 | 22525 | INSTRUMENTS AND FLIGHT RESEARCH INC. |
| 8317-13018 | 94271 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| 66-334 | 56232 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| CGH-10-AS-4 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CGC10AS4 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 8317-13018 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 11-800-00-002 | 78022 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE |
| 413265-1 | 96214 | RAYTHEON COMPANYDBA RAYTHEON |
| 8317-3223 | 23667 | SMITHS DETECTION, INC.DIV EDGEWOOD |
| 10515472 | 19200 | US ARMY ARDEC RDECOM |
Technical Data | NSN 5990-00-754-8135
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 148.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 600.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 27.50 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 174.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 7.70 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 30.50 NOMINAL |
| ZRS RESISTANCE IN OHMS | 47.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 16.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 16.60 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 7.30 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 5.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M6.0/P6.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 16.0 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.0 CENTIMETER-GRAMS MAXIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.6160 INCHES NOMINAL |
| FLANGE DIAMETER | 0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0630 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.8400 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0380 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES MAXIMUM |
| ALIGNMENT HOLE DEPTH | 0.0500 INCHES MAXIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.6780 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 3 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| FRAGILITY FACTOR | MODERATELY RUGGED |