NSN 5990-00-504-8795
Part Details | ELECTRICAL RESOLVER
5990-00-504-8795 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: 79143615, 791436-15, AY221S5B, 79143615, 791436-15, AY221S5B, AYS221S5B, 5990-00-504-8795, 00-504-8795, 5990005048795, 005048795
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-504-8795 | 22966 ( RESOLVER, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
2 ROTOR, 2 STATOR
Cross Reference | NSN 5990-00-504-8795
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 791436-15 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY221S5B | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 791436-15 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY221S5B | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AYS221S5B | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-504-8795
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 1.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 2.5 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 2.2 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 30.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 396.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 146.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 174.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 84.30 NOMINAL |
| ZRS RESISTANCE IN OHMS | 435.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 125.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 400.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 175.00 NOMINAL |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 5.00 INPUT |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M20.0/P20.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 5.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND B |
| 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 WIDTH | 0.0680 INCHES MINIMUM AND 0.0880 INCHES MAXIMUM |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| SHOULDER LENGTH | 0.1320 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.4590 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 7 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |
| SHAFT MAXIMUM RADIAL PLAY | 0.0010 INCHES |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT END PLAY | 0.0003 INCHES MINIMUM AND 0.0015 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| SCHEMATIC DIAGRAM DESIGNATOR | 1 2 ROTOR, 2 STATOR |
| FRAGILITY FACTOR | MODERATELY RUGGED |