NSN 5990-00-110-1153

Part Details | RECEIVER-TRANSMITTER SYNCHRO

5990-00-110-1153 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: 685021C300043, 685021C30004-3, 101732 PIECE 56, 10-1732 PIECE 56, 31TRX6A, M207086601A, M20708/66-01A, M2070866001, M20708/66-001, M2070866C001, M20708-66C-001, MILS2070866, MIL-S-20708/66, 15A4911, 15A491-1, 31TRX6, AS2070866, AS20708/66, AS2070899, AS20708/99, M207086601A, M20708/66-01A, 5990-00-110-1153, 00-110-1153, 5990001101153, 001101153

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59AUG 09, 196800-110-115327218 ( SYNCHRO, RECEIVER-TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND D

SYNCHRO,RECEIVER-TR | 5990-00-110-1153, 001101153
Cross Reference | NSN 5990-00-110-1153
Part Number Cage Code Manufacturer
685021C30004-396169ELECTRIC BOAT CORPORATION
10-1732 PIECE 5628199L3 TECHNOLOGIES, INC.DBA L3 HENSCHEL
31TRX6A81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/66-01A81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/66-00181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708-66C-00181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-20708/6681349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
15A491-103956NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS
31TRX613797ROCKWELL INTERNATIONAL CORPPOWER TOOL DIV INDUSTRIAL AIR TOOLS
AS20708/660VH01SAE CUSTOMER SERVICEDEPT 2045
AS20708/9981343SOCIETY OF AUTOMOTIVE ENGINEERS INC
M20708/66-01A81343SOCIETY OF AUTOMOTIVE ENGINEERS INC
Technical Data | NSN 5990-00-110-1153
Characteristic Specifications
BODY SIZE31
ROTOR INPUT VOLTAGE RATING IN VOLTS115.0 NOMINAL
ROTOR INPUT CURRENT RATING440.0 MILLIAMPERES MAXIMUM
ROTOR INPUT ELECTRICAL POWER RATING6.6 WATTS MAXIMUM
FREQUENCY IN HERTZ60.0 NOMINAL
ZSS IMPEDANCE MAGNITUDE IN OHMS24.00 MINIMUM AND 33.00 MAXIMUM
ZSS IMPEDANCE ANGLE IN DEG16.00 MINIMUM AND 24.00 MAXIMUM
TRANSFORMATION RATIO0.783 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG6.500 INPUT TO OUTPUT MAXIMUM
MAXIMUM TEMP RISE35.0 DEG CELSIUS
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT35.00 OUTPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT170.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM10.0/P10.0
RECEIVER ERROR ANGULAR RANGE IN MINUTESM36.0/P36.0
TORQUE GRADIENT PER ANGULAR DEG0.400 INCH-OUNCES MAXIMUM
BODY STYLE STANDARD ROUND D
SHOULDER DIAMETER2.6950 INCHES MINIMUM AND 2.7000 INCHES MAXIMUM
SECOND SHOULDER DIAMETER2.7500 INCHES MINIMUM AND 2.7510 INCHES MAXIMUM
SECOND SHOULDER LENGTH0.3750 INCHES NOMINAL
OVERALL LENGTH5.1000 INCHES NOMINAL
FLANGE DIAMETER2.0990 INCHES MINIMUM AND 3.1000 INCHES MAXIMUM
FLANGE THICKNESS0.2500 INCHES NOMINAL
BODY DIAMETER2.7000 INCHES MAXIMUM
PILOT LENGTH0.0300 INCHES NOMINAL
SHOULDER LENGTH0.6150 INCHES NOMINAL
AFT OF FIRST FLANGE DIAMETER2.7490 INCHES MINIMUM AND 2.7500 INCHES MAXIMUM
MOUNTING SURFACE TO TERMINAL END DISTANCE4.1200 INCHES NOMINAL
TERMINAL TYPE AND QUANTITY5 SCREW
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, CORROSION RESISTING
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 66 GOVERNMENT SPECIFICATION
FRAGILITY FACTOR MODERATELY RUGGED