NSN 5990-00-110-9441

Part Details | RECEIVER SYNCHRO


5990-00-110-9441 A synchro consisting of a stator and rotor inductively coupled. The rotor is free to turn in accordance with the electrical input from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, variable transformers, or items with dials.

Alternate Parts: M20708500001, M20708/500-001, 10TR4, M20708500001, M20708/500-001, MILS20708500, MIL-S-20708/500, 5990-00-110-9441, 00-110-9441, 5990001109441, 001109441

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JUN 27, 197300-110-944102072 ( SYNCHRO, RECEIVER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C


Cross Reference | NSN 5990-00-110-9441
Part Number Cage Code Manufacturer
M20708/500-00110112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
10TR481349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/500-00181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-20708/50081349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY

Technical Data | NSN 5990-00-110-9441
Characteristic Specifications
BODY SIZE10
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
ROTOR INPUT CURRENT RATING142.0 MILLIAMPERES MAXIMUM
ROTOR INPUT ELECTRICAL POWER RATING620.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZSS IMPEDANCE MAGNITUDE IN OHMS11.00 NOMINAL
ZSS IMPEDANCE ANGLE IN DEG15.000 NOMINAL
TRANSFORMATION RATIO0.454 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG7.500 INPUT TO OUTPUT MAXIMUM
MAXIMUM TEMP RISE20.0 DEG CELSIUS
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM60.0/P60.0
RECEIVER ERROR ANGULAR RANGE IN MINUTESM60.0/P60.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS2200.0 MILLIMETER-MILLIGRAMS NOMINAL
BODY STYLE STANDARD ROUND C
SHOULDER DIAMETER0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM
PILOT DIAMETER0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM
OVERALL LENGTH1.5460 INCHES MINIMUM AND 1.5760 INCHES MAXIMUM
FLANGE DIAMETER0.9360 INCHES MINIMUM AND 0.9380 INCHES MAXIMUM
FLANGE THICKNESS0.0620 INCHES NOMINAL
UNDERCUT DIAMETER0.8400 INCHES MAXIMUM
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0380 INCHES NOMINAL
SHOULDER LENGTH0.0620 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2400 INCHES MAXIMUM
ALIGNMENT HOLE DEPTH0.0625 INCHES MAXIMUM
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.6750 INCHES MINIMUM AND 0.6810 INCHES MAXIMUM
ALIGNMENT HOLE QUANTITY3
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
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 50 GOVERNMENT SPECIFICATION
ZSO-90 IMPEDANCE MAGNITUDE IN OHMS15.00 NOMINAL
FRAGILITY FACTOR MODERATELY RUGGED