Part Details | ELECTRICAL RESOLVER
5990-00-102-9600 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: 1R1SW4424C, 1R1SW4-424C, VRB15204A30, VRB15-204A30, 632338, MILR234178, MIL-R-23417/8, 1474922, 474922, 1474922, VRB15204A30, VRB15-20-4A30, 5990-00-102-9600, 00-102-9600, 5990001029600, 001029600
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JUN 03, 1968 | 00-102-9600 | 22966 ( RESOLVER, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
Cross Reference | NSN 5990-00-102-9600
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1R1SW4-424C | 08719 | DUCOMMUN LABARGE TECHNOLOGIES, INCDBA AMERICAN ELECTRONICS |
| VRB15-204A30 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| 632338 | 56232 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| MIL-R-23417/8 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 1474922 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 474922 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 1474922 | 53711 | NAVAL SEA SYSTEMS COMMAND |
| VRB15-20-4A30 | 10651 | VERNITRON CORP |
Technical Data | NSN 5990-00-102-9600
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 5.0 MINIMUM AND 26.0 MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZSO RESISTANCE IN OHMS | 480.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 2500.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 320.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 390.00 NOMINAL |
| TRANSFORMATION RATIO | 0.980 ROTOR TO STATOR NOMINAL |
| COMPENSATION METHOD | WINDING COMPENSATED |
| COMPENSATOR DC RESISTANCE IN OHMS | 520.00 NOMINAL |
| COMPENSATOR TRANSFORMATION RATIO IN PERCENT | 0.990 ROTOR TO COMPENSATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 8.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 15.00 OUTPUT |
| INTERAXIS ERROR ANGULAR RANGE IN MINUTES | M5.0/P5.0 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M0.1/P0.1 |
| BODY STYLE | STANDARD ROUND B |
| SHOULDER DIAMETER | 1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6745 INCHES MINIMUM AND 0.6750 INCHES MAXIMUM |
| OVERALL LENGTH | 2.6590 INCHES NOMINAL |
| FLANGE DIAMETER | 1.4320 INCHES MINIMUM AND 1.4390 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0950 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0750 INCHES NOMINAL |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| SHOULDER LENGTH | 0.1320 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.7870 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.1120 INCHES NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 1.1000 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 12 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| FRAGILITY FACTOR | MODERATELY RUGGED |