NSN 5990-00-501-2097
Part Details | ELECTRICAL RESOLVER
5990-00-501-2097 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: 11RP17, 11RP11, 11RC41, VRZ114CB63L, VRZ11-4CB63L, VRZ114CB62L, VRZ11-4CB62L, HQC11RQD9B225, HQC11RDG9B225, 577R708H11, 577R708H10, 5990-00-501-2097, 00-501-2097, 5990005012097, 005012097
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JUL 06, 1974 | 00-501-2097 | 22966 ( RESOLVER, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-501-2097
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 11RP17 | 08719 | DUCOMMUN LABARGE TECHNOLOGIES, INCDBA AMERICAN ELECTRONICS |
| 11RP11 | 08719 | DUCOMMUN LABARGE TECHNOLOGIES, INCDBA AMERICAN ELECTRONICS |
| 11RC41 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| VRZ11-4CB63L | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| VRZ11-4CB62L | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| HQC11RQD9B225 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| HQC11RDG9B225 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 577R708H11 | 97942 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN SYSTEMS |
| 577R708H10 | 97942 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN SYSTEMS |
Technical Data | NSN 5990-00-501-2097
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 15.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 22.0 MILLIAMPERES MAXIMUM |
| STATOR INPUT ELECTRICAL POWER RATING | 160.0 MILLIWATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 580.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 1630.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 370.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 1400.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 415.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 225.00 NOMINAL |
| TRANSFORMATION RATIO | 1.000 ROTOR TO STATOR NOMINAL |
| TRANSFORMATION RATIO EQUALITY IN PERCENT | 0.08 NOMINAL |
| COMPENSATION METHOD | RESISTOR COMPENSATED |
| COMPENSATOR DC RESISTANCE IN OHMS | 235.00 NOMINAL |
| COMPENSATOR TRANSFORMATION RATIO IN PERCENT | 0.080 ROTOR TO COMPENSATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 9.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 15.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 14.00 |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 0.07 INCH-OUNCES NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.9682 INCHES MINIMUM AND 0.9687 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 3.1200 INCHES NOMINAL |
| FLANGE DIAMETER | 1.0560 INCHES NOMINAL |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.9500 INCHES MINIMUM AND 0.9800 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0930 INCHES MINIMUM AND 0.1030 INCHES MAXIMUM |
| PILOT LENGTH | 0.0650 INCHES MAXIMUM |
| SHOULDER LENGTH | 0.0620 INCHES MINIMUM AND 0.0680 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6000 INCHES MINIMUM AND 2.2000 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 12 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| ZCO RESISTANCE IN OHMS | 370.00 NOMINAL |
| PLUS J ZCO REACTANCE IN OHMS | 1400.00 NOMINAL |
| FRAGILITY FACTOR | MODERATELY RUGGED |