NSN 5990-01-035-6869
Part Details | ELECTRICAL RESOLVER
5990-01-035-6869 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: 8RC300Y3, 8RC-300-Y-3, 14339001, 14339-001, ZL6A, ZL6-A, CM41034173, CM4-1034-173, CM41034173, CM4-1034-173, CSH8BA0004L902, CSH-8-BA-0004/L902, 755150231, 75515023-1, 755150231, 75515023-1, 5990-01-035-6869, 01-035-6869, 5990010356869, 010356869
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | FEB 12, 1977 | 01-035-6869 | 22966 ( RESOLVER, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-01-035-6869
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 8RC-300-Y-3 | 06989 | API HAROWE INCDBA API MOTION DIV API |
| 14339-001 | 10138 | ASTRONAUTICS CORPORATION OF AMERICA |
| ZL6-A | 51761 | CDA INTERCORP LLC |
| CM4-1034-173 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| CM4-1034-173 | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
| CSH-8-BA-0004/L902 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 75515023-1 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 75515023-1 | 1K426 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-01-035-6869
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 20.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 105.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 400.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 1550.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 300.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 1250.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 315.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 210.00 NOMINAL |
| TRANSFORMATION RATIO | 0.846 STATOR TO ROTOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 11.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 35.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.7500 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.7470 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.6880 INCHES MINIMUM AND 0.6910 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0380 INCHES MINIMUM AND 0.0430 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2400 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 7 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM ALLOY |
| FRAGILITY FACTOR | MODERATELY RUGGED |
