Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-914-0854 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: L03064, F498E131, F498E1-31, 18CT6, VTC18266A, VTC18-26-6A, VCT186N3, VCT18-6N3, 18CT6, 18CT60, 18CT6D, 18CT6B, 18CT6, M2070834C001, M20708/34C-001, M207083401D, M20708/34-01D, M2070834001, M20708-34-001, MILS2070834, MIL-S-20708/34, AS2070834, AS20708/34, AS2070834, AS20708/34, M207083401D, M20708/34-01D, 941B255, 18CT6B, 5990-00-914-0854, 00-914-0854, 5990009140854, 009140854
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1960 | 00-914-0854 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-914-0854
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| L03064 | 16236 | DLA LAND AND MARITIMEDBA ENGINEERING AND TECHNICAL |
| F498E1-31 | 81997 | EATON CORPCONTROLS DIV |
| 18CT6 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| VTC18-26-6A | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| VCT18-6N3 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| 18CT6 | 28199 | L3 TECHNOLOGIES, INC.DBA L3 HENSCHEL |
| 18CT60 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 18CT6D | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 18CT6B | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 18CT6 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/34C-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/34-01D | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708-34-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-20708/34 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| AS20708/34 | 0VH01 | SAE CUSTOMER SERVICEDEPT 2045 |
| AS20708/34 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| M20708/34-01D | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| 941B255 | 79500 | WESTINGHOUSE ELECTRIC CORP |
| 18CT6B | 79500 | WESTINGHOUSE ELECTRIC CORP |
Technical Data | NSN 5990-00-914-0854
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 18 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 90.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 17.0 MILLIAMPERES MAXIMUM |
| STATOR INPUT ELECTRICAL POWER RATING | 360.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 60.0 NOMINAL |
| ZSO IMPEDANCE MAGNITUDE IN OHMS | 4600.00 MINIMUM AND 5800.00 MAXIMUM |
| ZSO IMPEDANCE ANGLE IN DEG | 70.00 MINIMUM AND 76.00 MAXIMUM |
| ZRS IMPEDANCE MAGNITUDE IN OHMS | 1600.00 MINIMUM AND 2050.00 MAXIMUM |
| ZRS IMPEDANCE ANGLE IN DEG | 14.50 MINIMUM AND 18.00 MAXIMUM |
| TRANSFORMATION RATIO | 0.735 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 16.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 10.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 25.00 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 | 0.100 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 34 GOVERNMENT SPECIFICATION |
| FRAGILITY FACTOR | MODERATELY RUGGED |