NSN 5990-01-073-1640
Part Details | ELECTRICAL RESOLVER
5990-01-073-1640 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: MIS23529, MIS-23529, MIS23529, MIS-23529, CR40918043, 11R0731640, 11R073-1640, U217788, U-217788, MIS23529, MIS-23529, MIS23529, MIS-23529, 5990-01-073-1640, 01-073-1640, 5990010731640, 010731640
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | MAR 11, 1979 | 01-073-1640 | 22966 ( RESOLVER, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-01-073-1640
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| MIS-23529 | 08719 | DUCOMMUN LABARGE TECHNOLOGIES, INCDBA AMERICAN ELECTRONICS |
| MIS-23529 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| CR40918043 | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
| 11R073-1640 | 2X130 | MOTION DEVICES TECHNOLOGY, INC. |
| U-217788 | 82686 | TRANSICOIL LLCDBA ADS/TRANSICOIL |
| MIS-23529 | 82686 | TRANSICOIL LLCDBA ADS/TRANSICOIL |
| MIS-23529 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 5990-01-073-1640
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| FREQUENCY IN HERTZ | 470.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 92.00 MAXIMUM |
| PLUS J ZRO REACTANCE IN OHMS | 379.00 MAXIMUM |
| ZSO RESISTANCE IN OHMS | 100.00 MAXIMUM |
| PLUS J ZSO REACTANCE IN OHMS | 425.00 MAXIMUM |
| ZRS RESISTANCE IN OHMS | 140.00 MAXIMUM |
| PLUS J ZRS REACTANCE IN OHMS | 46.00 MAXIMUM |
| ZSS RESISTANCE IN OHMS | 157.00 MAXIMUM |
| PLUS J ZSS REACTANCE IN OHMS | 52.00 NOMINAL |
| TRANSFORMATION RATIO | 1.000 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 2.000 INPUT TO OUTPUT NOMINAL |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M2.0/P2.0 |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 6.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 2.6540 INCHES NOMINAL |
| FLANGE DIAMETER | 1.0600 INCHES NOMINAL |
| FLANGE THICKNESS | 0.0950 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.9750 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
| PILOT LENGTH | 0.0600 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0600 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 2.0900 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 8 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| SHAFT MAXIMUM RADIAL PLAY | 0.0010 INCHES |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT END PLAY | 0.0015 INCHES NOMINAL |
| SHAFT END PLAY DETERMINING WEIGHT | 16.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0014 INCHES |
| FRAGILITY FACTOR | MODERATELY RUGGED |
