Part Details | ELECTRICAL RESOLVER
5990-00-054-0512 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: 13846502, 138465-02, CSH8LA3L149, 5990-00-054-0512, 00-054-0512, 5990000540512, 000540512
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1961 | 00-054-0512 | 22966 ( RESOLVER, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-054-0512
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 138465-02 | 35351 | GE AVIATION SYSTEMS LLC |
| CSH8LA3L149 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-054-0512
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.00 NOMINAL |
| ROTOR INPUT CURRENT RATING | 15.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 110.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 916.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 2430.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 206.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 737.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 1210.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 258.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 725.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 160.00 NOMINAL |
| TRANSFORMATION RATIO | 0.478 ROTOR TO STATOR NOMINAL |
| TRANSFORMATION RATIO EQUALITY IN PERCENT | 3.5 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 17.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 6.0 DEG CELSIUS |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 60.00 |
| OUTPUT VOLTAGE FUNCTIONAL ERROR RANGE IN PERCENT | M7.0/P10.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.00 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.00 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.6000 INCHES MINIMUM AND 1.6400 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.5000 INCHES MINIMUM AND 0.7490 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.6910 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0430 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2405 INCHES MINIMUM AND 1.2410 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 7 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |