NSN 5990-00-553-5063
Part Details | ELECTRICAL RESOLVER
5990-00-553-5063 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: 59C871138REVB, AY221538B, AY2215-38B, AY221S38B, AY221S38, 35631520007, 3563152-0007, 12197752, 1219775-2, CS15DS1, CSC15DS3, CSC15DS1, 59C871138REVB, 666096423, 666096-423, 97605310, 976053-10, 10033251, 5990-00-553-5063, 00-553-5063, 5990005535063, 005535063
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-553-5063 | 22966 ( RESOLVER, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-553-5063
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 59C871138REVB | 1VPW8 | GENERAL DYNAMICS MISSION SYSTEMS,INC |
| AY2215-38B | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY221S38B | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY221S38 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 3563152-0007 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 1219775-2 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| CS15DS1 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CSC15DS3 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CSC15DS1 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 59C871138REVB | 94990 | MOTOROLA INC.DBA INTEGRATED INFORMATION SYSTEMS |
| 666096-423 | 57057 | NAVCOM DEFENSE ELECTRONICS, INC. |
| 976053-10 | 82577 | RAYTHEON COMPANYDBA RAYTHEON |
| 10033251 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 5990-00-553-5063
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 18.2 NOMINAL |
| STATOR INPUT CURRENT RATING | 14.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 60.0 MILLIWATTS NOMINAL |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 11.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 60.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 510.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 2500.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 250.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 1350.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 375.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 160.00 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 8.700 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M20.0/P20.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 30.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 10.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 2.1310 INCHES NOMINAL |
| FLANGE DIAMETER | 1.4360 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 1.3120 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0780 INCHES NOMINAL |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| SHOULDER LENGTH | 0.1320 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6310 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.5000 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 7 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |