Part Details | ELECTRICAL RESOLVER
5990-00-062-9482 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: 11R10B11B2, 11R10B11B-2, 11NHQ23RWZSF879, 11-NHQ-23RWZS/F879, 11NHQ23RWZSF879, 11-NHQ-23RWZS/F879, 11R0629482, 11R062-9482, 9170131, 5990-00-062-9482, 00-062-9482, 5990000629482, 000629482
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JUN 20, 1967 | 00-062-9482 | 22966 ( RESOLVER, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
Cross Reference | NSN 5990-00-062-9482
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 11R10B11B-2 | 08719 | DUCOMMUN LABARGE TECHNOLOGIES, INCDBA AMERICAN ELECTRONICS |
| 11-NHQ-23RWZS/F879 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 11-NHQ-23RWZS/F879 | 4H618 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 11R062-9482 | 2X130 | MOTION DEVICES TECHNOLOGY, INC. |
| 9170131 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 5990-00-062-9482
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 30.0 MILLIAMPERES NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZSO RESISTANCE IN OHMS | 160.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 880.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 145.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 91.00 NOMINAL |
| TRANSFORMATION RATIO | 0.980 ROTOR TO STATOR NOMINAL |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 0.40 INCH-OUNCES NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 0.22 INCH-OUNCES NOMINAL |
| BODY STYLE | STANDARD ROUND B |
| SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 2.4100 INCHES NOMINAL |
| FLANGE DIAMETER | 1.0610 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0900 INCHES MINIMUM AND 0.0960 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0470 INCHES MINIMUM AND 0.0670 INCHES MAXIMUM |
| PILOT LENGTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| SHOULDER LENGTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.8480 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8090 INCHES MINIMUM AND 0.8150 INCHES MAXIMUM |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 12 WIRE LEAD |
| TERMINAL LOCATION | SIDE |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| FRAGILITY FACTOR | MODERATELY RUGGED |