Part Details | ELECTRICAL RESOLVER
5990-00-124-2556 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: 55174, 9050503, 905050-3, AY084KJ111A1, 080V3408AL658, 080V3408A/L658, 5990-00-124-2556, 00-124-2556, 5990001242556, 001242556
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | NOV 15, 1968 | 00-124-2556 | 22966 ( RESOLVER, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
2 ROTOR, 2 STATOR
Cross Reference | NSN 5990-00-124-2556
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 55174 | 99479 | BOWMAR, LLC |
| 905050-3 | 05257 | GENERAL DYNAMICS LAND SYSTEMS-CANADA CORPORATION |
| AY084KJ111A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 080V3408A/L658 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-124-2556
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 66.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 416.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 158.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 490.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 44.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 150.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 263.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 75.50 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 133.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 36.30 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 15.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
| 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 A |
| PILOT DIAMETER | 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.4350 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.6910 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0430 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.0150 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 6 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| SHAFT MAXIMUM RADIAL PLAY | 0.0005 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 0.0008 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 8.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| SCHEMATIC DIAGRAM DESIGNATOR | 4 2 ROTOR, 2 STATOR |
| TERMINAL DESIGNATOR AND SCHEMATIC POSITION | CONNECTION R1 POSITION A AND CONNECTION R2 POSITION B AND CONNECTION S1 POSITION H AND CONNECTION S2 POSITION F AND CONNECTION S3 POSITION J AND CONNECTION S4 POSITION E |
| FRAGILITY FACTOR | MODERATELY RUGGED |