NSN 5990-00-926-4324

Part Details | RECEIVER-TRANSMITTER SYNCHRO

5990-00-926-4324 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: 23TRX6B, 23TRX6B, 23TRX6B, 23TRX6, 23TRX6A, 23TR6B, TRX236N3, TRX23-6N3, M207085601B, M20708/56-01B, 23TRX6B, 5M736098011, 5M7360-980-11, 22775340001, 2277534-0001, 23TRX6A, AY2401F12C2, 23TRX6, 5990PL0820496, 23TRX6, 491316900, 4913169-00, M2070856C001, M20708/56C-001, M207085601B, M20708/56-01B, MILS20708C1A56BM2070, MILS233581F, MIL-S-2335-8-1F, MILS2070856, MIL-S-20708/56, 8212778, 23TRX6B, 23TRX6, 23M4F1Q, 8151853085PC22, 815-1853085PC22, 2.012956, 59 000016, 59 000-016, AS2070856, AS20708/56, 512291, M207085601B, M20708/56-01B, AS2070856, AS20708/56, 5990-00-926-4324, 00-926-4324, 5990009264324, 009264324

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59MAY 09, 196600-926-432427218 ( SYNCHRO, RECEIVER-TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND D

Cross Reference | NSN 5990-00-926-4324
Part Number Cage Code Manufacturer
23TRX6BC0689CONSILIUM GMBH
23TRX6BS3012CONSILIUM MARINE & SAFETY AB,NAVIGATION
23TRX6BA135NCONSILIUM MARINE & SAFETY AB,NAVIGATION
23TRX612763DYNALEC CORPORATION
23TRX6A12763DYNALEC CORPORATION
23TR6B96169ELECTRIC BOAT CORPORATION
TRX23-6N310112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
M20708/56-01B10112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
23TRX6B10112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
5M7360-980-11D1901HENSOLDT SENSORS GMBHDIV SEPS
2277534-000102987HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX FLIGHT SYSTEMS
23TRX6A19315HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND
AY2401F12C255972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
23TRX612140INDEPENDENT PROTECTION CO INC
5990PL08204969009HINSPEKTORAT WSPARCIA SIL ZBROJNYCH
23TRX628199L3 TECHNOLOGIES, INC.DBA L3 HENSCHEL
4913169-0090536LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN
M20708/56C-00181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/56-01B81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MILS20708C1A56BM207081349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-2335-8-1F81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-20708/5681349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
821277881349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
23TRX6B81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
23TRX681349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
23M4F1QK0624MUIRHEAD AEROSPACE LTDDBA MUIRHEAD AVIONICS
815-1853085PC2280064NAVAL SHIP SYSTEMS COMMAND
2.012956D2865RAYTHEON ANSCHUETZ GMBHDBA RAYTHEON ELECTRICS GMBH
59 000-016D9853ROCKWELL COLLINS DEUTSCHLANDSERVICES GMBH
AS20708/560VH01SAE CUSTOMER SERVICEDEPT 2045
51229123667SMITHS DETECTION, INC.DIV EDGEWOOD
M20708/56-01B81343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AS20708/5681343SOCIETY OF AUTOMOTIVE ENGINEERS INC
Technical Data | NSN 5990-00-926-4324
Characteristic Specifications
BODY SIZE23
ROTOR INPUT VOLTAGE RATING IN VOLTS115.0 NOMINAL
ROTOR INPUT CURRENT RATING210.0 MILLIAMPERES MAXIMUM
ROTOR INPUT ELECTRICAL POWER RATING5.6 WATTS MAXIMUM
FREQUENCY IN HERTZ60.0 NOMINAL
ZSS IMPEDANCE MAGNITUDE IN OHMS110.00 MINIMUM AND 145.00 MAXIMUM
ZSS IMPEDANCE ANGLE IN DEG10.00 MINIMUM AND 17.00 MAXIMUM
TRANSFORMATION RATIO0.783 STATOR TO ROTOR NOMINAL
PHASE SHIFT ANGLE IN DEG11.000 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE35.0 DEG CELSIUS
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT60.00 OUTPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT160.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM8.0/P8.0
RECEIVER ERROR ANGULAR RANGE IN MINUTESM45.0/P45.0
TORQUE GRADIENT PER ANGULAR DEG0.120 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 DIAMETER1.9400 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 56 GOVERNMENT SPECIFICATION
FRAGILITY FACTOR MODERATELY RUGGED