NSN 5990-00-073-1760
Part Details | ELECTRICAL TRANSOLVER
5990-00-073-1760 An item consisting of a rotor and a stator inductively coupled. It has wye connected and quadrature windings, either of which can be stator or the rotor and serve as the Primary for input voltages. The output voltages are trigonometric functions of the input voltages and the angular displacement of the rotor with respect to the stator. See also SYNCHRO (as modified). Excludes RESOLVER, ELECTRICAL and potentiometer sine/cosine electrical resolvers.
Alternate Parts: 68C40009, 10CRD100B1, 13770201, 137702-01, CL40902002, CL40902002, 71569041, 7156904-1, 7156904, 5072781, 507278-1, 5990-00-073-1760, 00-073-1760, 5990000731760, 000731760
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-073-1760 | 33272 ( TRANSOLVER, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-073-1760
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 68C40009 | 97151 | AIR FORCE LIFECYCLE MANAGEMENTCENTER ELECTRONIC COMPONENTS |
| 10CRD100B1 | 06989 | API HAROWE INCDBA API MOTION DIV API |
| 137702-01 | 35351 | GE AVIATION SYSTEMS LLC |
| CL40902002 | 09301 | KEARFOTT CORP SOMA FORWARDING DIV |
| CL40902002 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| 7156904-1 | 1NZ85 | L3 TECHNOLOGIES, INC.DBA SPACE AND NAVIGATION |
| 7156904 | 1NZ85 | L3 TECHNOLOGIES, INC.DBA SPACE AND NAVIGATION |
| 507278-1 | 96214 | RAYTHEON COMPANYDBA RAYTHEON |
Technical Data | NSN 5990-00-073-1760
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 42.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 103.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 85.40 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 281.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 77.60 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 363.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 84.30 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 31.10 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 75.50 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 41.00 NOMINAL |
| TRANSFORMATION RATIO | 1.041 STATOR TO ROTOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 10.800 OUTPUT TO INPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 6.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 1.0000 INCHES NOMINAL |
| PILOT DIAMETER | 0.5000 INCHES NOMINAL |
| OVERALL LENGTH | 1.6280 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.9370 INCHES NOMINAL |
| FLANGE THICKNESS | 0.1250 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.8123 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0380 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2400 INCHES MAXIMUM |
| ALIGNMENT HOLE DEPTH | 0.1000 INCHES NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.6780 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 3 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| SPECIAL FEATURES | RESOLVER IS CRITICAL FOR FIT FORM AND FUNCTION TOLERANCE AND APPLICATION FOR THE AMPLIFIER POWER SUPPLY FOR THE E-3 AIRCRAFT |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| FRAGILITY FACTOR | MODERATELY RUGGED |