NSN 5990-00-135-6180

Part Details | DIFFERENTIAL TRANSMITTER SYNCHRO

5990-00-135-6180 A synchro, the rotor of which is mechanically positioned for modifying electrical angular information, received from a transmitter synchro and transmitting to receiver synchro or control transformer synchro electrical information corresponding to the sum or difference of the electrical input angle and its rotor position angle. Does not include variable resistors, goniometers, variable transformers, or items with dials.

Alternate Parts: VCDX156N2, VCDX15-6N2, 15CDX6C, M207082201C, M20708/22-01C, MILS2070822, MILS20708-22, 15CDX6B, 5990-00-135-6180, 00-135-6180, 5990001356180, 001356180

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 13, 196900-135-618002071 ( SYNCHRO, DIFFERENTIAL TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

Cross Reference | NSN 5990-00-135-6180
Part Number Cage Code Manufacturer
VCDX15-6N210112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
15CDX6C81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/22-01C81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MILS20708-2281349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
15CDX6B80048VICKERS INCELECTRIC PRODUCTS DIVISION
Technical Data | NSN 5990-00-135-6180
Characteristic Specifications
BODY SIZE15
STATOR INPUT VOLTAGE RATING IN VOLTS90.0 NOMINAL
STATOR INPUT CURRENT RATING38.0 MILLIAMPERES MAXIMUM
STATOR INPUT ELECTRICAL POWER RATING500.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ60.0 NOMINAL
ZSO IMPEDANCE MAGNITUDE IN OHMS2050.00 MINIMUM AND 2600.00 MINIMUM
ZSO IMPEDANCE ANGLE IN DEG77.00 MINIMUM AND 83.00 MAXIMUM
ZRS IMPEDANCE MAGNITUDE IN OHMS900.00 MINIMUM AND 1200.00 MAXIMUM
ZRS IMPEDANCE ANGLE IN DEG11.00 MINIMUM AND 17.00 MAXIMUM
TRANSFORMATION RATIO1.154 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG9.000 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE20.0 DEG CELSIUS
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT60.00 OUTPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT100.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM7.0/P7.0
TORQUE GRADIENT PER ANGULAR DEG0.070 INCH-OUNCES MAXIMUM
BODY STYLE STANDARD ROUND C
SHOULDER DIAMETER1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM
PILOT DIAMETER0.8745 INCHES MINIMUM AND 0.8750 INCHES MAXIMUM
OVERALL LENGTH3.2220 INCHES NOMINAL
FLANGE DIAMETER1.4367 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM
FLANGE THICKNESS0.0930 INCHES NOMINAL
UNDERCUT DIAMETER1.3120 INCHES NOMINAL
UNDERCUT WIDTH0.0780 INCHES NOMINAL
PILOT LENGTH0.0400 INCHES NOMINAL
SHOULDER LENGTH0.1320 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE2.6820 INCHES NOMINAL
ALIGNMENT HOLE DEPTH0.1250 INCHES MINIMUM
ALIGNMENT HOLE BOLT CIRCLE DIAMETER1.1000 INCHES NOMINAL
ALIGNMENT HOLE QUANTITY4
TERMINAL TYPE AND QUANTITY6 SCREW
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, STAINLESS
TEST DATA DOCUMENT81349-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 DATA81349-MIL--20708 TO 22 GOVERNMENT SPECIFICATION
FRAGILITY FACTOR MODERATELY RUGGED