NSN 5990-00-924-4167
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-924-4167 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: 18CT4, 15CT6D, M20708504001, M20708/504-001, M2070821A001, M20708/21A-001, M207082101D, M20708/21-01D, M2070821001, M20708/21-001, MILS2070821, MIL-S-20708/21, M207082101D, M20708/21-01D, AS207082101D, AS20708/21-01D, AS2070821, AS20708/21, 1998307, 5990-00-924-4167, 00-924-4167, 5990009244167, 009244167
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 20, 1966 | 00-924-4167 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-924-4167
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 18CT4 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 15CT6D | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/504-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/21A-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/21-01D | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/21-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-20708/21 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/21-01D | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AS20708/21-01D | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AS20708/21 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| 1998307 | 56289 | SPRAGUE ELECTRIC COWORLD HQS |
Technical Data | NSN 5990-00-924-4167
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 90.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 13.0 MILLIAMPERES MAXIMUM |
| STATOR INPUT ELECTRICAL POWER RATING | 210.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 60.0 NOMINAL |
| ZSO IMPEDANCE MAGNITUDE IN OHMS | 6000.00 MINIMUM AND 7500.00 MAXIMUM |
| ZSO IMPEDANCE ANGLE IN DEG | 78.00 MINIMUM AND 82.00 MAXIMUM |
| ZRS IMPEDANCE MAGNITUDE IN OHMS | 1300.00 MINIMUM AND 1650.00 MAXIMUM |
| ZRS IMPEDANCE ANGLE IN DEG | 1300.00 MINIMUM AND 1800.00 MAXIMUM |
| TRANSFORMATION RATIO | 0.735 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 9.000 INPUT TO OUTPUT MAXIMUM |
| MAXIMUM TEMP RISE | 10.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 65.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 45.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M6.0/P6.0 |
| TORQUE GRADIENT PER ANGULAR DEG | 0.050 INCH-OUNCES MAXIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM |
| PILOT DIAMETER | 0.8745 INCHES MINIMUM AND 0.8750 INCHES MAXIMUM |
| OVERALL LENGTH | 3.0630 INCHES NOMINAL |
| FLANGE DIAMETER | 1.4320 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 1.3120 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 | 2.5230 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES MINIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 1.1000 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 21 GOVERNMENT SPECIFICATION |
| FRAGILITY FACTOR | MODERATELY RUGGED |
