6625-01-032-0709 LEAD,TEST Index 5990-01-032-0711 STATOR,SYNCHRO

National Stock Number:
5990-01-032-0710

Federal Supply Class:
5990

National Item Identification Number:
010320710

Description:
SYNCHRO,TRANSMITTER

Detail:
A SYNCHRO CONSISTING OF A STATOR AND ROTOR INDUCTIVELY COUPLED. THE ELECTRICAL OUTPUT OF THE STATOR INTO A RECEIVER SYNCHRO, A CONTROL TRANSFORMER OR DIFFERENTIAL SYNCHRO IS DEPENDENT UPON THE POSITION OF ITS ROTOR. DOES NOT INCLUDE VARIABLE RESISTORS, GONIOMETERS, VARIABLE TRANSFORMERS, OR ITEMS WITH DIALS.


Manufacturer Information:
11CX4E81349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
26-11TX481349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
26V-11TX4C05088KEARFOTT CORP
AS20708/60U583SAE INTERNATIONAL
AS20708/60VH01SAE CUSTOMER SERVICE DEPT 2045
AS20708/681343SOCIETY OF AUTOMOTIVE ENGINEERS INC
M20708/6-00299932MOOG INC.
M20708/6-02C0U583SAE INTERNATIONAL
M20708/6-02C81343SOCIETY OF AUTOMOTIVE ENGINEERS INC
M20708/6-02C81349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
M20708/6D-00281349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
MIL-S-20708/681349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
SAE-AS20708/60U583SAE INTERNATIONAL


Techincal Specification:
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES-7.0 TO 7.0
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS0.07 INCH-OUNCES MAXIMUM
ALIGNMENT HOLE QUANTITY4
BODY MATERIALSTEEL CORROSION RESISTING
BODY SIZE11
BODY STYLESTANDARD ROUND B
FLANGE DIAMETER1.0570 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM
FLANGE THICKNESS0.0930 INCHES NOMINAL
FRAGILITY FACTORMODERATELY RUGGED
FREQUENCY IN HERTZ400.0 NOMINAL
OVERALL LENGTH3.3720 INCHES MAXIMUM
MAXIMUM TEMP RISE20.0 CELSIUS
MOUNTING SURFACE TO TERMINAL END DISTANCE1.6520 INCHES NOMINAL
PILOT DIAMETER0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM
PHASE SHIFT ANGLE IN DEG4.000 INPUT TO OUTPUT NOMINAL
PILOT LENGTH0.0620 INCHES NOMINAL
PLUS J ZSS REACTANCE IN OHMS17.00 MINIMUM AND 24.00 MAXIMUM
ROTOR INPUT CURRENT RATING280.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING1.0 WATTS NOMINAL
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
SHAFT DIAMETER0.1200 INCHES NOMINAL SINGLE SHAFT
SHAFT LENGTH0.3680 INCHES NOMINAL SINGLE SHAFT
SHAFT SLOT DEPTH0.0250 INCHES NOMINAL SINGLE SHAFT
SHAFT SLOT WIDTH0.0200 INCHES NOMINAL SINGLE SHAFT
SHAFT TYPEROUND, SLOTTED SINGLE SHAFT
SHOULDER DIAMETER0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM
SHOULDER LENGTH0.0620 INCHES NOMINAL
SPECIFICATION/STANDARD DATA81349-MIL-S-20708/6 GOVERNMENT SPECIFICATION
ZSS RESISTANCE IN OHMS3.30 MINIMUM AND 4.20 MAXIMUM
TERMINAL LOCATIONREAR
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
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 DEG0.008 INCH-OUNCES MINIMUM
TRANSFORMATION RATIO0.454 ROTOR TO STATOR NOMINAL
UNDERCUT WIDTH0.0620 INCHES NOMINAL


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