NSN 5990-00-851-4363
Part Details | ELECTRICAL RESOLVER
5990-00-851-4363 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: 11R10B11B, 11R10B-11B, R40957, VRW114CF53L, VRW11-4CF-53L, 11NLQ23RWZSF901, 11-NLQ-23RWZS/F901, 11NLQ23RWZSF901, 11-NLQ-23RWZS/F901, 11R8514363, 11R851-4363, 10066427, 10043609, 5990-00-851-4363, 00-851-4363, 5990008514363, 008514363
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1962 | 00-851-4363 | 22966 ( RESOLVER, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-851-4363
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 11R10B-11B | 08719 | DUCOMMUN LABARGE TECHNOLOGIES, INCDBA AMERICAN ELECTRONICS |
| R40957 | 08719 | DUCOMMUN LABARGE TECHNOLOGIES, INCDBA AMERICAN ELECTRONICS |
| VRW11-4CF-53L | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| 11-NLQ-23RWZS/F901 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 11-NLQ-23RWZS/F901 | 4H618 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 11R851-4363 | 2X130 | MOTION DEVICES TECHNOLOGY, INC. |
| 10066427 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
| 10043609 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 5990-00-851-4363
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 26.0 MAXIMUM |
| STATOR INPUT CURRENT RATING | 30.0 MILLIAMPERES MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 160.00 NOMINAL |
| PLUS J ZRO 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 |
| COMPENSATION METHOD | WINDING COMPENSATED |
| COMPENSATOR DC RESISTANCE IN OHMS | 370.00 NOMINAL |
| COMPENSATOR TRANSFORMATION RATIO IN PERCENT | 0.985 ROTOR TO COMPENSATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 6.600 INPUT TO OUTPUT NOMINAL |
| INTERAXIS ERROR ANGULAR RANGE IN MINUTES | M5.0/P5.0 |
| OUTPUT VOLTAGE FUNCTIONAL ERROR RANGE IN PERCENT | M0.1/P0.1 |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 2.3950 INCHES MINIMUM AND 2.4250 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.0610 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0900 INCHES MINIMUM AND 0.0960 INCHES MAXIMUM |
| UNDERCUT DIAMETER | 0.9720 INCHES MINIMUM AND 0.9780 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 | 1.9100 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 12 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| FRAGILITY FACTOR | MODERATELY RUGGED |
