NSN 5990-00-905-1836

Part Details | TRANSMITTER SYNCHRO

5990-00-905-1836 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: 15CX1249, VCX154NB2, VCX15-4NB2, 7745191P006, BUWEPSDWG2625501, M207081401D, M20708/14-01D, M2070814001, M20708/14-001, M2070814E001, M20708-14E001, MILS2070814, MIL-S-20708/14, 15CX4D, 15CX4D, 2625501, 1803743, 632443, 15CY6B, AS20708, 1803743, 5990-00-905-1836, 00-905-1836, 5990009051836, 009051836

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 01, 196000-905-183602073 ( SYNCHRO, TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

Cross Reference | NSN 5990-00-905-1836
Part Number Cage Code Manufacturer
15CX124914404AMETEK TECHNICAL & INDUSTRIALPRODUCTS, INC.
VCX15-4NB210112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
7745191P00603538LOCKHEED MARTIN CORPORATIONDIV RMS
BUWEPSDWG262550136090LOCKHEED MARTIN LIBRASCOPECORP
M20708/14-01D81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/14-00181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708-14E00181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-20708/1481349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
15CX4D81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
15CX4D99932MOOG INC.DBA MOOG COMPONENTS GROUP
262550110001NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT
180374310001NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT
63244303956NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS
15CY6B03956NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS
AS207080VH01SAE CUSTOMER SERVICEDEPT 2045
180374331143ZENITRON MFG CORPDBA NORTHEAST MFG CO
Technical Data | NSN 5990-00-905-1836
Characteristic Specifications
BODY SIZE15
ROTOR INPUT VOLTAGE RATING IN VOLTS115.0 NOMINAL
ROTOR INPUT CURRENT RATING85.0 MILLIAMPERES MAXIMUM
ROTOR INPUT ELECTRICAL POWER RATING1.0 WATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO IMPEDANCE MAGNITUDE IN OHMS1402.00 MINIMUM AND 1643.00 MAXIMUM
ZRO IMPEDANCE ANGLE IN DEG81.40 MINIMUM AND 84.60 MAXIMUM
ZSS IMPEDANCE MAGNITUDE IN OHMS123.00 MINIMUM AND 138.00 MAXIMUM
ZSS IMPEDANCE ANGLE IN DEG26.50 MINIMUM AND 31.50 MAXIMUM
TRANSFORMATION RATIO0.783 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG4.000 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE20.0 DEG CELSIUS
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT32.00 OUTPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT60.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM6.0/P6.0
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS0.05 INCH-OUNCES MAXIMUM
BODY STYLE STANDARD ROUND C
SHOULDER DIAMETER1.3070 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM
PILOT DIAMETER0.8745 INCHES MINIMUM AND 0.8750 INCHES MAXIMUM
OVERALL LENGTH2.3120 INCHES NOMINAL
FLANGE DIAMETER1.4320 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 DISTANCE1.7720 INCHES NOMINAL
TERMINAL TYPE AND QUANTITY5 SCREW
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, CORROSION RESISTING
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 14 GOVERNMENT SPECIFICATION
FRAGILITY FACTOR MODERATELY RUGGED