NSN 5990-00-928-5593
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-928-5593 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the rotor is dependent upon both the position of the rotor and the electrical input to the stator from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, or variable transformers.
Alternate Parts: 18CT4B, 18CT4C, 18CT4, 18CT4A, W41281A6000A10, W41281-A6000-A10, M207082901C, M20708/29-01C, M207082901, M20708-29-01, M2070829001, M20708-29-001, MILS2070829, MIL-S-20708/29, 18CT4C, 18CT4B, M207829D001, M2078/29D-001, 4509049153, 450904-9153, 3151268P2, 315-1268P2, S3151268P2, S315-1268P2, V23401C0003A010, M207082901C, M20708/29-01C, AS2070829, AS20708/29, 5990-00-928-5593, 00-928-5593, 5990009285593, 009285593
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | AUG 31, 1966 | 00-928-5593 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-928-5593
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 18CT4B | 08160 | BOWEN & COMPANY INC.DBA |
| 18CT4C | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| 18CT4 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| 18CT4A | 98853 | HAMILTON STANDARD ELECTRONICSSYSTEMS INC |
| W41281-A6000-A10 | C0426 | HENSOLDT SENSORS GMBH |
| M20708/29-01C | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708-29-01 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708-29-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-20708/29 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 18CT4C | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 18CT4B | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M2078/29D-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 450904-9153 | D4856 | NORTHROP GRUMMAN LITEF GMBHDBA LITEF |
| 315-1268P2 | 99687 | RAYTHEON CO EQUIPMENT DEVELOPMENTLAB |
| S315-1268P2 | 99687 | RAYTHEON CO EQUIPMENT DEVELOPMENTLAB |
| V23401C0003A010 | C0425 | SIEMENS AG EC R LOG |
| M20708/29-01C | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AS20708/29 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 5990-00-928-5593
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 18 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 90.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 7.0 MILLIAMPERES MAXIMUM |
| STATOR INPUT ELECTRICAL POWER RATING | 50.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZSO IMPEDANCE MAGNITUDE IN OHMS | 12000.00 MINIMUM AND 14800.00 MAXIMUM |
| ZSO IMPEDANCE ANGLE IN DEG | 82.00 MINIMUM AND 84.50 MAXIMUM |
| ZRS IMPEDANCE MAGNITUDE IN OHMS | 980.00 MINIMUM AND 1180.00 MAXIMUM |
| ZRS IMPEDANCE ANGLE IN DEG | 42.00 MINIMUM AND 52.00 MAXIMUM |
| TRANSFORMATION RATIO | 0.735 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 2.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 20.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 20.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M6.0/P6.0 |
| TORQUE GRADIENT PER ANGULAR DEG | 0.100 INCH-OUNCES MAXIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 1.5615 INCHES MINIMUM AND 1.5620 INCHES MAXIMUM |
| PILOT DIAMETER | 0.9370 INCHES MINIMUM AND 0.9375 INCHES MAXIMUM |
| OVERALL LENGTH | 3.0600 INCHES NOMINAL |
| FLANGE DIAMETER | 1.7450 INCHES MINIMUM AND 1.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 1.6250 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0780 INCHES NOMINAL |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| SHOULDER LENGTH | 0.1320 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 2.5200 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES MINIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 1.2500 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| TEST DATA DOCUMENT | 81349-MIL-S-20708 SPECIFICATION (INCLUDES ENGINEERING TYPE BULLETINS, BROCHURES,ETC., THAT REFLECT SPECIFICATION TYPE DATA IN SPECIFICATION FORMAT; EXCLUDES COMMERCIAL CATALOGS, INDUSTRY DIRECTORIES, AND SIMILAR TRADE PUBLICATIONS, REFLECTING GENERAL TYPE DATA ON CERTAIN ENVIRONMENTAL AND PERFORMANCE REQUIREMENTS AND TEST CONDITIONS THAT ARE SHOWN AS "TYPICAL", "AVERAGE", "NOMINAL", ETC.). |
| SPECIFICATION/STANDARD DATA | 81349-MIL--20708 TO 29 GOVERNMENT SPECIFICATION |
