NSN 5990-00-945-9914

Part Details | DIFFERENTIAL TRANSMITTER SYNCHRO

5990-00-945-9914 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: 15CDX1142, 7674782, VCDX154NB2, VCDX15-4NB2, AY1531A3B2, 15CDX4, M2070816001, M20708-16-001, 15CX4A, 15CDX4D, 15CDX4B, M207081601D, M20708/16-01D, M2070816001, M20708-16-001, MILS2070816, MIL-S-20708/16, 15CDX4D, N20024, 7674782, 5990-00-945-9914, 00-945-9914, 5990009459914, 009459914

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59MAR 14, 196600-945-991402071 ( SYNCHRO, DIFFERENTIAL TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

Cross Reference | NSN 5990-00-945-9914
Part Number Cage Code Manufacturer
15CDX114214404AMETEK TECHNICAL & INDUSTRIALPRODUCTS, INC.
767478210112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
VCDX15-4NB210112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
AY1531A3B255972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
15CDX428199L3 TECHNOLOGIES, INC.DBA L3 HENSCHEL
M20708-16-00156232LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN
15CX4A81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
15CDX4D81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
15CDX4B81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/16-01D81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708-16-00181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-20708/1681349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
15CDX4D97942NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN SYSTEMS
N2002481574TCE CANADA LTD
767478219200US ARMY ARDEC RDECOM
Technical Data | NSN 5990-00-945-9914
Characteristic Specifications
BODY SIZE15
STATOR INPUT VOLTAGE RATING IN VOLTS90.0 NOMINAL
STATOR INPUT CURRENT RATING90.0 MILLIAMPERES MAXIMUM
STATOR INPUT ELECTRICAL POWER RATING900.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZSO IMPEDANCE MAGNITUDE IN OHMS870.00 MINIMUM AND 1150.00 MAXIMUM
ZSO IMPEDANCE ANGLE IN DEG79.00 MINIMUM AND 85.00 MAXIMUM
ZRS IMPEDANCE MAGNITUDE IN OHMS195.00 MINIMUM AND 290.00 MAXIMUM
ZRS IMPEDANCE ANGLE IN DEG27.00 MINIMUM AND 37.00 MAXIMUM
TRANSFORMATION RATIO1.154 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG5.500 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
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 LENGTH2.4700 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 DISTANCE1.9300 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--20708-16 GOVERNMENT SPECIFICATION
FRAGILITY FACTOR MODERATELY RUGGED