NSN 5990-00-295-7068
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-295-7068 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: 10CT1151, D7289612, D728961-2, 10CT0155B, 10CT-0155-B, 7289612, 728961-2, 7289612, 728961-2, AY5035A1, AY503-5A1, 7185042, 718504-2, AY5035AL, AY503-5AL, 10CT2957068, 10CT295-7068, 5990-00-295-7068, 00-295-7068, 5990002957068, 002957068
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-295-7068 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
Cross Reference | NSN 5990-00-295-7068
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 10CT1151 | 14404 | AMETEK TECHNICAL & INDUSTRIALPRODUCTS, INC. |
| D728961-2 | 06840 | BENDIX CORP THE |
| 10CT-0155-B | 51761 | CDA INTERCORP LLC |
| 728961-2 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 728961-2 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY503-5A1 | 55973 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 718504-2 | 56232 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| AY503-5AL | 56232 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| 10CT295-7068 | 2X130 | MOTION DEVICES TECHNOLOGY, INC. |
Technical Data | NSN 5990-00-295-7068
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 9.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 12.0 WATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 920.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 2100.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 220.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 445.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 1090.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 445.00 NOMINAL |
| TRANSFORMATION RATIO | 1.850 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 15.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 0.05 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M15.0/P15.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND B |
| SHOULDER DIAMETER | 0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.6540 INCHES NOMINAL |
| FLANGE DIAMETER | 0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 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 | 1.1790 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.0630 INCHES NOMINAL |
| 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, STAINLESS |
| FRAGILITY FACTOR | MODERATELY RUGGED |