NSN 5990-00-607-0117
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-607-0117 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the rotor is dependent upon both the position of the rotor and the electrical input to the stator from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, or variable transformers.
Alternate Parts: CR40901090, HTC11E8F128, HTC-11-E-8/F128, HTC11E8F128, HTC-11-E-8/F128, 101A271, 3157022P1, 315-7022P1, U205267, U-205267, 9190983, 9072872, 5990-00-607-0117, 00-607-0117, 5990006070117, 006070117
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-607-0117 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-607-0117
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CR40901090 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| HTC-11-E-8/F128 | 4H618 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| HTC-11-E-8/F128 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 101A271 | 21877 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVAL AND MARINE SYSTEMS |
| 315-7022P1 | 49956 | RAYTHEON COMPANYDBA RAYTHEON |
| U-205267 | 82686 | TRANSICOIL LLCDBA ADS/TRANSICOIL |
| 9190983 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
| 9072872 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 5990-00-607-0117
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 90.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 20.0 MILLIAMPERES MAXIMUM |
| STATOR INPUT ELECTRICAL POWER RATING | 180.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO IMPEDANCE MAGNITUDE IN OHMS | 3340.00 NOMINAL |
| ZRO IMPEDANCE ANGLE IN DEG | 79.20 NOMINAL |
| ZSO IMPEDANCE MAGNITUDE IN OHMS | 5470.00 NOMINAL |
| ZSO IMPEDANCE ANGLE IN DEG | 80.80 NOMINAL |
| ZRS IMPEDANCE MAGNITUDE IN OHMS | 718.00 NOMINAL |
| TRANSFORMATION RATIO | 0.735 ROTOR TO STATOR NOMINAL |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 59.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 94.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M10.0/P10.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 16.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 2.1290 INCHES MINIMUM AND 2.1530 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.0570 INCHES MINIMUM AND 1.0650 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.9750 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 | 1.7650 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |