NSN 5990-00-276-8650

Part Details | CONTROL TRANSFORMER SYNCHRO

5990-00-276-8650 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: VCT154N2, VCT15-4N2, MILS2070815, MIL-S-20708/15, 15CT4C, M207081502C, M20708/15-02C, 15CT4C, AS2070815, AS20708/15, 5990-00-276-8650, 00-276-8650, 5990002768650, 002768650

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59AUG 08, 197300-276-865015289 ( SYNCHRO, CONTROL TRANSFORMER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

SYNCHRO,CONTROL TRA | 5990-00-276-8650, 002768650
Cross Reference | NSN 5990-00-276-8650
Part Number Cage Code Manufacturer
VCT15-4N210112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
MIL-S-20708/1581349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
15CT4C81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/15-02C81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
15CT4C99932MOOG INC.DBA MOOG COMPONENTS GROUP
AS20708/150VH01SAE CUSTOMER SERVICEDEPT 2045
Technical Data | NSN 5990-00-276-8650
Characteristic Specifications
BODY SIZE15
STATOR INPUT VOLTAGE RATING IN VOLTS90.0 NOMINAL
STATOR INPUT CURRENT RATING10.0 MILLIAMPERES MAXIMUM
STATOR INPUT ELECTRICAL POWER RATING140.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZSO IMPEDANCE MAGNITUDE IN OHMS7800.00 MINIMUM AND 9512.00 MAXIMUM
ZSO IMPEDANCE ANGLE IN DEG77.80 MINIMUM AND 84.50 MAXIMUM
ZRS IMPEDANCE MAGNITUDE IN OHMS1050.00 MINIMUM AND 1300.00 MAXIMUM
ZRS IMPEDANCE ANGLE IN DEG26.00 MINIMUM AND 33.00 MAXIMUM
TRANSFORMATION RATIO0.735 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG5.500 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE10.0 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 DEG0.050 INCH-OUNCES MAXIMUM
BODY STYLE STANDARD ROUND C
SHOULDER DIAMETER1.3116 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
ALIGNMENT HOLE DEPTH0.1250 INCHES NOMINAL
ALIGNMENT HOLE BOLT CIRCLE DIAMETER1.1000 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 15 GOVERNMENT SPECIFICATION
FRAGILITY FACTOR MODERATELY RUGGED