NSN 5990-00-976-9496
Part Details | ELECTRICAL RESOLVER
5990-00-976-9496 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: 10RC103A1, 1064262G1, AY54357A2, AY543-57A2, AY54357A2, AY543-57A2, 406314, 4063-14, CWH10MS3A151, CVH10MS5A285, 5990-00-976-9496, 00-976-9496, 5990009769496, 009769496
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1962 | 00-976-9496 | 22966 ( RESOLVER, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-976-9496
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 10RC103A1 | 06989 | API HAROWE INCDBA API MOTION DIV API |
| 1064262G1 | 28527 | HARRIS CORPORATIONDBA ELECTRONIC SYSTEMS, INTEGRATED |
| AY543-57A2 | 55973 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY543-57A2 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 4063-14 | 58880 | MEGGITT (NEW HAMPSHIRE), INC |
| CWH10MS3A151 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CVH10MS5A285 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-976-9496
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 3.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 30.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 55.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 135.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 60.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 87.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 890.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 1350.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 550.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 770.00 NOMINAL |
| TRANSFORMATION RATIO | 3.000 STATOR TO ROTOR NOMINAL |
| TRANSFORMATION RATIO EQUALITY IN PERCENT | 3.0 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 36.000 INPUT TO OUTPUT MAXIMUM |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 25.0 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 5.0 CENTIMETER-GRAMS MAXIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.6590 INCHES NOMINAL |
| FLANGE DIAMETER | 0.9370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.8350 INCHES MINIMUM AND 0.8400 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0380 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2460 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 6 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| SHAFT MAXIMUM RADIAL PLAY | 0.0008 INCHES |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 40.0 GRAMS |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| FRAGILITY FACTOR | MODERATELY RUGGED |
