NSN 5990-00-455-9865
Part Details | ELECTRICAL RESOLVER
5990-00-455-9865 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: 1116001P1, RS9312G, RS931-2G, 5990-00-455-9865, 00-455-9865, 5990004559865, 004559865
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | APR 25, 1969 | 00-455-9865 | 22966 ( RESOLVER, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
2 ROTOR, 2 STATOR
Cross Reference | NSN 5990-00-455-9865
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1116001P1 | 94117 | BAE SYSTEMS INFORMATION ANDELECTRONIC SYSTEMS INTEGRATION INC. |
| RS931-2G | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
Technical Data | NSN 5990-00-455-9865
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 520.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 340.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO IMPEDANCE MAGNITUDE IN OHMS | 550.00 NOMINAL |
| ZRO IMPEDANCE ANGLE IN DEG | 78.10 NOMINAL |
| ZSO IMPEDANCE MAGNITUDE IN OHMS | 150.00 NOMINAL |
| ZSO IMPEDANCE ANGLE IN DEG | 80.30 NOMINAL |
| ZRS IMPEDANCE MAGNITUDE IN OHMS | 159.50 NOMINAL |
| ZRS IMPEDANCE ANGLE IN DEG | 24.70 NOMINAL |
| TRANSFORMATION RATIO | 484.000 STATOR TO ROTOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 8.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 18.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| 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 | 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 2.3720 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.0620 INCHES NOMINAL |
| 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 | 1.7030 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 7 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 | 0.0005 INCHES MINIMUM AND 0.0015 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 16.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0008 INCHES |
| SCHEMATIC DIAGRAM DESIGNATOR | 3 2 ROTOR, 2 STATOR |
| TERMINAL DESIGNATOR AND SCHEMATIC POSITION | CONNECTION R1 POSITION B AND CONNECTION R2 POSITION A AND CONNECTION R3 POSITION C AND CONNECTION S1 POSITION J AND CONNECTION S2 POSITION F AND CONNECTION S3 POSITION H AND CONNECTION S4 POSITION E |
| FRAGILITY FACTOR | MODERATELY RUGGED |