NSN 5990-00-988-7902

Part Details | CONTROL TRANSFORMER SYNCHRO

5990-00-988-7902 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: 18CX1256, VCX186N1, VCX18-6N1, M2070833C001, M20708/33C-001, M207083301C, M20708/33-01C, M2070833001, M20708/33-001, MILS2070833C, MIL-S-20708/33C, MILS2070833, MIL-S-20708/33, 18CX6C, 2.013028, 4186800039, 4186800-039, 59 000015, 59 000-015, 191599, V23401C0006A009, M207083301C, M20708/33-01C, AS2070833, AS20708/33, 18CX6C, 5990-00-988-7902, 00-988-7902, 5990009887902, 009887902

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59NOV 02, 196600-988-790215289 ( SYNCHRO, CONTROL TRANSFORMER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

Cross Reference | NSN 5990-00-988-7902
Part Number Cage Code Manufacturer
18CX125614404AMETEK TECHNICAL & INDUSTRIALPRODUCTS, INC.
VCX18-6N110112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
M20708/33C-00181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/33-01C81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/33-00181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-20708/33C81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-20708/3381349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
18CX6C81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
2.013028D2865RAYTHEON ANSCHUETZ GMBHDBA RAYTHEON ELECTRICS GMBH
4186800-03905869RAYTHEON COMPANYDBA RAYTHEON
59 000-015D9853ROCKWELL COLLINS DEUTSCHLANDSERVICES GMBH
19159910110SCIENTIFIC ATLANTA INC
V23401C0006A009C0425SIEMENS AG EC R LOG
M20708/33-01C81343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AS20708/3381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
18CX6CD2416THALES DEFENCE & SECURITYSYSTEMSGMBH
Technical Data | NSN 5990-00-988-7902
Characteristic Specifications
BODY SIZE18
STATOR INPUT VOLTAGE RATING IN VOLTS115.0 NOMINAL
STATOR INPUT CURRENT RATING40.0 MILLIAMPERES MAXIMUM
STATOR INPUT ELECTRICAL POWER RATING950.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ60.0 NOMINAL
ZRO IMPEDANCE MAGNITUDE IN OHMS2875.00 MINIMUM AND 3375.00 MAXIMUM
ZRO IMPEDANCE ANGLE IN DEG76.00 MINIMUM AND 80.00 MAXIMUM
ZSS IMPEDANCE MAGNITUDE IN OHMS660.00 MINIMUM AND 810.00 MAXIMUM
ZSS IMPEDANCE ANGLE IN DEG9.00 MINIMUM AND 13.00 MAXIMUM
TRANSFORMATION RATIO0.783 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG11.000 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE25.0 DEG CELSIUS
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT30.00 OUTPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT85.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM8.0/P8.0
TORQUE GRADIENT PER ANGULAR DEG0.100 INCH-OUNCES MAXIMUM
BODY STYLE STANDARD ROUND C
SHOULDER DIAMETER1.5615 INCHES MINIMUM AND 1.5620 INCHES MAXIMUM
PILOT DIAMETER0.9370 INCHES MINIMUM AND 0.9375 INCHES MAXIMUM
OVERALL LENGTH3.0600 INCHES NOMINAL
FLANGE DIAMETER1.7450 INCHES MINIMUM AND 1.7500 INCHES MAXIMUM
FLANGE THICKNESS0.0930 INCHES NOMINAL
UNDERCUT DIAMETER1.6250 INCHES NOMINAL
UNDERCUT WIDTH0.0780 INCHES NOMINAL
PILOT LENGTH0.0400 INCHES NOMINAL
SHOULDER LENGTH0.1320 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE2.5200 INCHES NOMINAL
ALIGNMENT HOLE DEPTH0.1250 INCHES MINIMUM
ALIGNMENT HOLE BOLT CIRCLE DIAMETER1.2500 INCHES NOMINAL
ALIGNMENT HOLE QUANTITY4
TERMINAL TYPE AND QUANTITY5 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 33 GOVERNMENT SPECIFICATION
FRAGILITY FACTOR MODERATELY RUGGED