5355-00-881-1029 KNOB Index 5340-00-881-1033 PLATE,MOUNTING

National Stock Number:
5990-00-881-1031

Federal Supply Class:
5990

National Item Identification Number:
008811031

Description:
SYNCHRO,CONTROL TRANSFORMER

Detail:
A SYNCHRO CONSISTING OF A STATOR AND ROTOR INDUCTIVELY COUPLED. THE ELECTRICAL OUTPUT OF THE ROTOR IS DEPENDENT UPON BOTH THE POSITION OF THE ROTOR AND THE ELECTRICAL INPUT TO THE STATOR FROM A TRANSMITTER SYNCHRO OR A DIFFERENTIAL SYNCHRO. DOES NOT INCLUDE VARIABLE RESISTORS, GONIOMETERS, OR VARIABLE TRANSFORMERS.


Manufacturer Information:
138A91600103956NORTHROP GRUMMAN SYSTEMS CORPORATION
26V-08CT4C/79-01C99932MOOG INC.
AS20708/790U583SAE INTERNATIONAL
AS20708/790VH01SAE CUSTOMER SERVICE DEPT 2045
26V08CT4C81349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
710190093322GE AVIATION SYSTEMS LLC DBA GE AVIATION
M20708/79-01C0U583SAE INTERNATIONAL
SAE-AS20708/790U583SAE INTERNATIONAL
AS20708/7981343SOCIETY OF AUTOMOTIVE ENGINEERS INC
M20708/79-01C81343SOCIETY OF AUTOMOTIVE ENGINEERS INC
M20708/79-01C81349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
MILS20708-7981349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
M20708-79D-00181349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
M20708/79-00181349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M


Techincal Specification:
BODY SIZE8
BODY STYLESTANDARD ROUND A
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES-7.0 TO 7.0
FLANGE DIAMETER0.7450 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM
FLANGE THICKNESS0.0620 INCHES NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
PHASE SHIFT ANGLE IN DEG8.000 INPUT TO OUTPUT NOMINAL
PILOT DIAMETER0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM
PILOT LENGTH0.0400 INCHES NOMINAL
MATERIALSTEEL CORROSION RESISTING BODY
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT25.00 OUTPUT
MAXIMUM TEMP RISE10.0 CELSIUS
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT30.00
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2400 INCHES MAXIMUM
OVERALL LENGTH1.5920 INCHES NOMINAL
SHAFT DIAMETER0.0898 INCHES MINIMUM AND 0.0900 INCHES MAXIMUM SINGLE SHAFT
SHAFT SLOT DEPTH0.0250 INCHES NOMINAL SINGLE SHAFT
SHAFT SLOT WIDTH0.0200 INCHES NOMINAL SINGLE SHAFT
SHAFT TYPEROUND, SLOTTED SINGLE SHAFT
SHAFT LENGTH0.3520 INCHES NOMINAL SINGLE SHAFT
SPECIFICATION/STANDARD DATA81349-MIL-S-20708/79 GOVERNMENT SPECIFICATION
STATOR INPUT CURRENT RATING23.0 MILLIAMPERES MAXIMUM
STATOR INPUT ELECTRICAL POWER RATING44.0 MILLIWATTS NOMINAL
STATOR INPUT VOLTAGE RATING IN VOLTS11.8 NOMINAL
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 DEG0.040 INCH-OUNCES MAXIMUM
TRANSFORMATION RATIO2.203 ROTOR TO STATOR NOMINAL
UNDERCUT WIDTH0.0620 INCHES NOMINAL
UNDERCUT DIAMETER0.6870 INCHES NOMINAL
ZRO IMPEDANCE ANGLE IN DEG16.00 MINIMUM AND 20.00 MAXIMUM
ZRO IMPEDANCE MAGNITUDE IN OHMS830.00 MINIMUM AND 940.00 MAXIMUM
ZSO IMPEDANCE ANGLE IN DEG76.00 MINIMUM AND 81.00 MAXIMUM
ZSO IMPEDANCE MAGNITUDE IN OHMS444.00 MINIMUM AND 570.00 MAXIMUM


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