NSN 5990-00-878-1909
Part Details | ELECTRICAL RESOLVER
5990-00-878-1909 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: 8RC300K30B, 189123000, 189123-000, 189122000, 189122-000, 088400Z, 088-400Z, W1623B226, W1623B2-26, W1623B226, W1623B2-26, W1623B126, W1623B1-26, 088400Z, 088-400Z, W1623B226, W1623B2-26, HSC8AH7L061, HSC8AH7L229, HSC-8-AH-7-L229, VR08124A1, VR08-12-4A1, 5990-00-878-1909, 00-878-1909, 5990008781909, 008781909
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-878-1909 | 22966 ( RESOLVER, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-878-1909
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 8RC300K30B | 06989 | API HAROWE INCDBA API MOTION DIV API |
| 189123-000 | 81413 | BAE SYSTEMS INFORMATION ANDELECTRONIC SYSTEMS INTEGRATION I |
| 189122-000 | 81413 | BAE SYSTEMS INFORMATION ANDELECTRONIC SYSTEMS INTEGRATION I |
| 088-400Z | 99743 | IMC MAGNETICS CORPWESTERN DIV |
| W1623B2-26 | 99743 | IMC MAGNETICS CORPWESTERN DIV |
| W1623B2-26 | 07421 | INTERSTATE ELECTRONICS CORPORATIONDBA L-3 INTERSTATE ELECTRONICS |
| W1623B1-26 | 07421 | INTERSTATE ELECTRONICS CORPORATIONDBA L-3 INTERSTATE ELECTRONICS |
| 088-400Z | 92703 | KEMTRON ELECTRON PRODUCTS INC |
| W1623B2-26 | 92703 | KEMTRON ELECTRON PRODUCTS INC |
| HSC8AH7L061 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| HSC-8-AH-7-L229 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| VR08-12-4A1 | 10651 | VERNITRON CORP |
Technical Data | NSN 5990-00-878-1909
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 0.5 MINIMUM AND 16.5 MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 522.75 MINIMUM AND 707.25 MAXIMUM |
| PLUS J ZRO REACTANCE IN OHMS | 1232.50 MINIMUM AND 1667.50 MAXIMUM |
| ZSO RESISTANCE IN OHMS | 85.00 MINIMUM AND 115.00 MAXIMUM |
| PLUS J ZSO REACTANCE IN OHMS | 246.45 MINIMUM AND 333.55 MAXIMUM |
| ZRS RESISTANCE IN OHMS | 697.00 MINIMUM AND 943.00 MAXIMUM |
| PLUS J ZRS REACTANCE IN OHMS | 161.50 MINIMUM AND 218.50 MAXIMUM |
| TRANSFORMATION RATIO | 0.400 ROTOR TO STATOR MINIMUM AND 0.416 ROTOR TO STATOR MAXIMUM |
| PHASE SHIFT ANGLE IN DEG | 19.500 INPUT TO OUTPUT MINIMUM AND 22.500 INPUT TO OUTPUT MAXIMUM |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 20.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 25.00 |
| INTERAXIS ERROR ANGULAR RANGE IN MINUTES | M15.0/P15.0 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M14.0/P14.0 |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.6070 INCHES MINIMUM AND 1.6450 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.7470 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| UNDERCUT DIAMETER | 0.6880 INCHES MINIMUM AND 0.6910 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| PILOT LENGTH | 0.0370 INCHES MINIMUM AND 0.0430 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2900 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 7 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ANY ACCEPTABLE |
| FRAGILITY FACTOR | MODERATELY RUGGED |
