NSN 5990-00-519-3421

Part Details | TRANSMITTER SYNCHRO

5990-00-519-3421 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the stator into a receiver synchro, a control transformer or differential synchro is dependent upon the position of its rotor. Does not include variable resistors, goniometers, variable transformers, or items with dials.

Alternate Parts: 8212778, 23TX6A, 23TC6A, 23TC6A, 760147100, 76-01471-00, 760147100, 76-01471-00, 23TX6A, 5M736098012, 5M7360-980-12, 23TX6A, MILS12472TYPE23TX6A, MS510801, MS51080-1, 23TX6A, D10930, B201F8212778, VBM281, VBM2-81, 5990-00-519-3421, 00-519-3421, 5990005193421, 005193421

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 01, 196300-519-342102073 ( SYNCHRO, TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND D

Cross Reference | NSN 5990-00-519-3421
Part Number Cage Code Manufacturer
821277819204ARMY, UNITED STATES DEPARTMENT OFTHE
23TX6AA135NCONSILIUM MARINE & SAFETY AB,NAVIGATION
23TC6AS3012CONSILIUM MARINE & SAFETY AB,NAVIGATION
23TC6AA135NCONSILIUM MARINE & SAFETY AB,NAVIGATION
76-01471-00S3012CONSILIUM MARINE & SAFETY AB,NAVIGATION
76-01471-00A135NCONSILIUM MARINE & SAFETY AB,NAVIGATION
23TX6AS3012CONSILIUM MARINE & SAFETY AB,NAVIGATION
5M7360-980-12D1901HENSOLDT SENSORS GMBHDIV SEPS
23TX6AD1901HENSOLDT SENSORS GMBHDIV SEPS
MILS12472TYPE23TX6A81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MS51080-196906MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS
23TX6AK0624MUIRHEAD AEROSPACE LTDDBA MUIRHEAD AVIONICS
D1093095542NORTHROP GRUMMAN SYSTEMS CORPORATION
B201F821277892755NORTHROP GRUMMAN SYSTEMS CORPORATIONDBA LAND & SELF PROTECTION SYSTEM
VBM2-81H0203THALES NEDERLANDDBA THALES LAND & JOINT SYSTEMS
Technical Data | NSN 5990-00-519-3421
Characteristic Specifications
BODY SIZE23
ROTOR INPUT VOLTAGE RATING IN VOLTS115.0 NOMINAL
ROTOR INPUT CURRENT RATING210.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING5.0 WATTS NOMINAL
FREQUENCY IN HERTZ60.0 NOMINAL
ZRO RESISTANCE IN OHMS132.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS494.00 NOMINAL
ZSO RESISTANCE IN OHMS98.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS311.00 NOMINAL
ZRS RESISTANCE IN OHMS249.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS79.00 NOMINAL
ZSO-90 RESISTANCE IN OHMS94.00 NOMINAL
PLUS J ZSO-90 REACTANCE IN OHMS113.00 NOMINAL
TRANSFORMATION RATIO0.783 ROTOR TO STATOR NOMINAL
MAXIMUM TEMP RISE65.0 DEG CELSIUS
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM8.0/P8.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS0.50 INCH-OUNCES MAXIMUM
TORQUE GRADIENT PER ANGULAR DEG0.130 INCH-OUNCES NOMINAL
BODY STYLE STANDARD ROUND D
SHOULDER DIAMETER1.9980 INCHES MINIMUM AND 1.9990 INCHES MAXIMUM
PILOT DIAMETER0.5900 INCHES MINIMUM AND 0.6000 INCHES MAXIMUM
SECOND SHOULDER DIAMETER1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM
SECOND SHOULDER LENGTH0.1720 INCHES NOMINAL
OVERALL LENGTH4.2430 INCHES MINIMUM AND 4.2940 INCHES MAXIMUM
FLANGE DIAMETER2.2490 INCHES MINIMUM AND 2.2500 INCHES MAXIMUM
FLANGE THICKNESS0.2500 INCHES NOMINAL
BODY DIAMETER1.9850 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM
PILOT LENGTH0.0460 INCHES NOMINAL
SHOULDER LENGTH0.2500 INCHES NOMINAL
AFT OF FIRST FLANGE DIAMETER1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM
MOUNTING SURFACE TO TERMINAL END DISTANCE3.4350 INCHES MINIMUM AND 3.4450 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY7 SCREW
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, CORROSION RESISTING
TEST DATA DOCUMENT81349-MIL-S-12472 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--12472 GOVERNMENT SPECIFICATION