NSN 5990-00-677-6476
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-677-6476 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: 16CTB4B, VTCB164C2, VTCB16-4C2, MILS2070825, MIL-S-20708/25, MILS20708, MIL-S-20708, 21930252, 2193025-2, 222172, 22217-2, 5990-00-677-6476, 00-677-6476, 5990006776476, 006776476
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | JAN 01, 1963 | 00-677-6476 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
Cross Reference | NSN 5990-00-677-6476
Part Number | Cage Code | Manufacturer |
---|---|---|
16CTB4B | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
VTCB16-4C2 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
MIL-S-20708/25 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
MIL-S-20708 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
2193025-2 | 30003 | NAVAL AIR SYSTEMS COMMAND MANAGEDORIGINAL DESIGN ACTIVITY NOT |
22217-2 | 10412 | WHITTAKER CORPWHITTAKER ELECTRONIC SYSTEMS DIV |
Technical Data | NSN 5990-00-677-6476
Characteristic | Specifications |
---|---|
BODY SIZE | 16 |
STATOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
STATOR INPUT CURRENT RATING | 24.0 MILLIAMPERES NOMINAL |
STATOR INPUT ELECTRICAL POWER RATING | 600.0 MILLIWATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
TRANSFORMATION RATIO | 0.735 ROTOR TO STATOR NOMINAL |
PHASE SHIFT ANGLE IN DEG | 8.000 INPUT TO OUTPUT NOMINAL |
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 40.00 OUTPUT |
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 60.00 |
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M10.0/P10.0 |
TORQUE GRADIENT PER ANGULAR DEG | 0.050 INCH-OUNCES MAXIMUM |
BODY STYLE | STANDARD ROUND B |
SHOULDER DIAMETER | 1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM |
PILOT DIAMETER | 0.8745 INCHES MINIMUM AND 0.8750 INCHES MAXIMUM |
OVERALL LENGTH | 3.1330 INCHES MAXIMUM |
FLANGE DIAMETER | 1.5320 INCHES MINIMUM AND 1.5410 INCHES MAXIMUM |
FLANGE THICKNESS | 0.0900 INCHES MINIMUM AND 0.0960 INCHES MAXIMUM |
UNDERCUT WIDTH | 0.0730 INCHES MINIMUM AND 0.0830 INCHES MAXIMUM |
PILOT LENGTH | 0.0370 INCHES MINIMUM AND 0.0430 INCHES MAXIMUM |
SHOULDER LENGTH | 0.1270 INCHES MINIMUM AND 0.1370 INCHES MAXIMUM |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 2.5775 INCHES MINIMUM AND 2.5780 INCHES MAXIMUM |
TERMINAL TYPE AND QUANTITY | 5 SCREW |
TERMINAL LOCATION | REAR |
BODY MATERIAL | STEEL, CORROSION RESISTING |
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 25 GOVERNMENT SPECIFICATION |