5920-00-110-1152 FUSE,CARTRIDGE Index 5998-00-110-1154 PRINTED CIRCUIT BOARD

National Stock Number:
5990-00-110-1153

Federal Supply Class:
5990

National Item Identification Number:
001101153

Description:
SYNCHRO,RECEIVER-TRANSMITTER

Detail:
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.


Manufacturer Information:
10-1732 PIECE 5628199L3 TECHNOLOGIES, INC.
15A491-103956NORTHROP GRUMMAN SYSTEMS CORPORATION
31TRX613797ROCKWELL INTERNATIONAL CORP POWER TOOL DIV INDUSTRIAL AIR TOOLS
31TRX6A81349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
685021C30004-396169ELECTRIC BOAT CORPORATION
AS20708/660VH01SAE CUSTOMER SERVICE DEPT 2045
AS20708/990U583SAE INTERNATIONAL
AS20708/9981343SOCIETY OF AUTOMOTIVE ENGINEERS INC
M20708-66C-00181349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
M20708/66-00181349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
M20708/66-01A0U583SAE INTERNATIONAL
M20708/66-01A81343SOCIETY OF AUTOMOTIVE ENGINEERS INC
M20708/66-01A81349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
MIL-S-20708/6681349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
SAE-AS20708/660U583SAE INTERNATIONAL
SAE-AS20708?/660U583SAE INTERNATIONAL


Techincal Specification:
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES-10.0 TO 10.0
AFT OF FIRST FLANGE DIAMETER2.7490 INCHES MINIMUM AND 2.7500 INCHES MAXIMUM
BODY DIAMETER2.7000 INCHES MAXIMUM
BODY MATERIALSTEEL, CORROSION RESISTING
BODY SIZE31
BODY STYLESTANDARD ROUND D
FLANGE DIAMETER2.0990 INCHES MINIMUM AND 3.1000 INCHES MAXIMUM
FLANGE THICKNESS0.2500 INCHES NOMINAL
FRAGILITY FACTORMODERATELY RUGGED
FREQUENCY IN HERTZ60.0 NOMINAL
OVERALL LENGTH5.1000 INCHES NOMINAL
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT35.00 OUTPUT
MAXIMUM TEMP RISE35.0 CELSIUS
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT170.00
MOUNTING SURFACE TO TERMINAL END DISTANCE4.1200 INCHES NOMINAL
PHASE SHIFT ANGLE IN DEG6.500 INPUT TO OUTPUT MAXIMUM
PILOT LENGTH0.0300 INCHES NOMINAL
RECEIVER ERROR ANGULAR RANGE IN MINUTES-36.0 TO 36.0
ROTOR INPUT CURRENT RATING440.0 MILLIAMPERES MAXIMUM
ROTOR INPUT ELECTRICAL POWER RATING6.6 WATTS MAXIMUM
ROTOR INPUT VOLTAGE RATING IN VOLTS115.0 NOMINAL
SECOND SHOULDER DIAMETER2.7500 INCHES MINIMUM AND 2.7510 INCHES MAXIMUM
SECOND SHOULDER LENGTH0.3750 INCHES NOMINAL
SHAFT DIAMETER0.2403 INCHES MINIMUM AND 0.2405 INCHES MAXIMUM SINGLE SHAFT
SHAFT LENGTH0.7300 INCHES NOMINAL SINGLE SHAFT
SHAFT NOMINAL THREAD SIZE0.250 INCHES SINGLE SHAFT
SHAFT THREAD CLASS2A SINGLE SHAFT
SHAFT THREAD DIRECTIONRIGHT-HAND SINGLE SHAFT
SHAFT THREAD LENGTH0.3100 INCHES NOMINAL SINGLE SHAFT
SHAFT THREAD SERIES DESIGNATORUNF SINGLE SHAFT
SHAFT TYPESPLINE W/THREADS SINGLE SHAFT
SHOULDER DIAMETER2.6950 INCHES MINIMUM AND 2.7000 INCHES MAXIMUM
SHOULDER LENGTH0.6150 INCHES NOMINAL
SPECIFICATION/STANDARD DATA81349-MIL-S-20708/66 GOVERNMENT SPECIFICATION
SPLINE TOOTH DIAMETRAL PITCH96 SINGLE SHAFT
SPLINE TOOTH QUANTITY22 SINGLE SHAFT
ZSS IMPEDANCE ANGLE IN DEG16.00 MINIMUM AND 24.00 MAXIMUM
ZSS IMPEDANCE MAGNITUDE IN OHMS24.00 MINIMUM AND 33.00 MAXIMUM
TERMINAL LOCATIONREAR
TERMINAL TYPE AND QUANTITY5 SCREW
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.).
TORQUE GRADIENT PER ANGULAR DEG0.400 INCH-OUNCES MAXIMUM
TRANSFORMATION RATIO0.783 ROTOR TO STATOR NOMINAL


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