NSN 5990-00-519-5758
Part Details | ELECTRICAL RESOLVER
5990-00-519-5758 An item consisting of a rotor and a stator inductively coupled. It usually has two rotor windings displaced from each other by 90 degrees and two stator windings similarly displaced. The output voltage(s) is a trigonometric function of the input voltage(s) and the angular displacement of the rotor with respect to the stator. See also SYNCHRO (as modified) and GONIOMETER, ELECTRICAL. Excludes TRANSOLVER, ELECTRICAL and potentiometer sine/cosine electrical resolvers.
Alternate Parts: 4501077, 450-1077, 134437000, 134437-000, 100938000, 100938-000, AY52325A1, AY523-25A1, 2102209, 210-2209, AY52325A1, AY523-25A1, 10406109, 10-4061-09, CSC10MS1, CSC-10-MS-1, 1JC78405, 1JC7840-5, 1JC78405, 1JC7840-5, 5990-00-519-5758, 00-519-5758, 5990005195758, 005195758
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-519-5758 | 22966 ( RESOLVER, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
Cross Reference | NSN 5990-00-519-5758
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 450-1077 | 81413 | BAE SYSTEMS INFORMATION ANDELECTRONIC SYSTEMS INTEGRATION I |
| 134437-000 | 81413 | BAE SYSTEMS INFORMATION ANDELECTRONIC SYSTEMS INTEGRATION I |
| 100938-000 | 81413 | BAE SYSTEMS INFORMATION ANDELECTRONIC SYSTEMS INTEGRATION I |
| AY523-25A1 | 06840 | BENDIX CORP THE |
| 210-2209 | 94486 | COSMOS INDUSTRIES INC |
| AY523-25A1 | 19315 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND |
| 10-4061-09 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CSC-10-MS-1 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 1JC7840-5 | 97942 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN SYSTEMS |
| 1JC7840-5 | 79500 | WESTINGHOUSE ELECTRIC CORP |
Technical Data | NSN 5990-00-519-5758
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 40.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 450.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 268.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 620.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 70.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 188.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 210.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 12.00 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 17.000 INPUT TO OUTPUT NOMINAL |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M12.0/P12.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 25.00 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 7.0 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 | 0.0630 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.1780 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.0620 INCHES NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.6780 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 3 |
| TERMINAL TYPE AND QUANTITY | 7 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |