NSN 5990-00-904-3314

Part Details | RECEIVER-TRANSMITTER SYNCHRO

5990-00-904-3314 A synchro having a dual purpose. It may be used in applications requiring either a receiver or transmitter. For synchros having a single purpose, see SYNCHRO, RECEIVER and SYNCHRO, TRANSMITTER.

Alternate Parts: 23TRX4A, VSSC2236P12, MILS2070850BM20708, MILS20708-50BM20708-, MILS2070844, MILS20708-44, MILS2070850, MIL-S-20708/50, 23TRX4A, 23TRX4, M207850C001, M2078/50C-001, M2070850D001, M20708/50D-001, M207085001A, M20708/50-01A, M2070850C001, M20708-50C-001, M2070850001, M20708-50-001, 23M4F2Q, AS2070850, AS20708/50, M207085001A, M20708/50-01A, VTRX234N3, VTRX23/4N3, 5990-00-904-3314, 00-904-3314, 5990009043314, 009043314

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JUN 17, 196600-904-331427218 ( SYNCHRO, RECEIVER-TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND D

Cross Reference | NSN 5990-00-904-3314
Part Number Cage Code Manufacturer
23TRX4A10112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
VSSC2236P1210112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
MILS20708-50BM20708-81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MILS20708-4481349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-20708/5081349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
23TRX4A81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
23TRX481349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M2078/50C-00181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/50D-00181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/50-01A81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708-50C-00181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708-50-00181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
23M4F2QK0624MUIRHEAD AEROSPACE LTDDBA MUIRHEAD AVIONICS
AS20708/5081343SOCIETY OF AUTOMOTIVE ENGINEERS INC
M20708/50-01A81343SOCIETY OF AUTOMOTIVE ENGINEERS INC
VTRX23/4N310651VERNITRON CORP
Technical Data | NSN 5990-00-904-3314
Characteristic Specifications
BODY SIZE23
ROTOR INPUT VOLTAGE RATING IN VOLTS115.0 NOMINAL
ROTOR INPUT CURRENT RATING720.0 MILLIAMPERES MAXIMUM
FREQUENCY IN HERTZ400.0 NOMINAL
ZSS IMPEDANCE MAGNITUDE IN OHMS6.50 MINIMUM AND 8.10 MAXIMUM
ZSS IMPEDANCE ANGLE IN DEG42.00 MINIMUM AND 46.00 MAXIMUM
TRANSFORMATION RATIO0.783 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG2.000 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE30.0 DEG CELSIUS
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT30.00 OUTPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT150.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM6.0/P6.0
RECEIVER ERROR ANGULAR RANGE IN MINUTESM45.0/P45.0
TORQUE GRADIENT PER ANGULAR DEG0.250 INCH-OUNCES MINIMUM
BODY STYLE STANDARD ROUND D
SHOULDER DIAMETER1.9850 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM
PILOT DIAMETER0.5950 INCHES NOMINAL
SECOND SHOULDER DIAMETER1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM
SECOND SHOULDER LENGTH0.1700 INCHES NOMINAL
OVERALL LENGTH4.2990 INCHES NOMINAL
FLANGE DIAMETER2.2490 INCHES MINIMUM AND 2.2500 INCHES MAXIMUM
FLANGE THICKNESS0.2500 INCHES NOMINAL
BODY DIAMETER1.9900 INCHES MAXIMUM
PILOT LENGTH0.0430 INCHES NOMINAL
SHOULDER LENGTH0.2500 INCHES NOMINAL
AFT OF FIRST FLANGE DIAMETER1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM
MOUNTING SURFACE TO TERMINAL END DISTANCE3.5800 INCHES NOMINAL
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 50 GOVERNMENT SPECIFICATION
FRAGILITY FACTOR MODERATELY RUGGED