5962-00-465-4826 MICROCIRCUIT,DIGITAL Index 5990-00-465-4832 SYNCHRO,TRANSMITTER

National Stock Number:
5990-00-465-4829

Federal Supply Class:
5990

National Item Identification Number:
004654829

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:
1289134H618MOOG INC.
26V-08CX4C81349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
AS20708/780VH01SAE CUSTOMER SERVICE DEPT 2045
710190193322GE AVIATION SYSTEMS LLC DBA GE AVIATION
531500-196214RAYTHEON COMPANY
26V-08CX4C/78-01C99932MOOG INC.
M20708/78-01C0U583SAE INTERNATIONAL
SAE-AS20708/780U583SAE INTERNATIONAL
M20708/78-01C81349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
MIL-S-20708/7881349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
M20708-78D00181349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
M20708/78-00181349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M


Techincal Specification:
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS0.04 INCH-OUNCES MAXIMUM
BODY MATERIALSTEEL CORROSION RESISTING
BODY SIZE8
BODY STYLESTANDARD ROUND A
CRITICALITY CODE JUSTIFICATIONFEAT
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES-7.0 TO 7.0
FLANGE DIAMETER0.7470 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM
FLANGE THICKNESS0.0620 INCHES NOMINAL
FRAGILITY FACTORMODERATELY RUGGED
FREQUENCY IN HERTZ400.0 NOMINAL
PILOT LENGTH0.0400 INCHES NOMINAL
PHASE SHIFT ANGLE IN DEG8.500 INPUT TO OUTPUT NOMINAL
PILOT DIAMETER0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT20.00 OUTPUT
MAXIMUM TEMP RISE20.0 CELSIUS
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT30.00
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2400 INCHES MAXIMUM
OVERALL LENGTH1.6050 INCHES NOMINAL
ROTOR INPUT CURRENT RATING153.0 MILLIAMPERES MAXIMUM
ROTOR INPUT ELECTRICAL POWER RATING700.0 MILLIWATTS NOMINAL
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
SHAFT LENGTH0.3650 INCHES NOMINAL SINGLE SHAFT
SHAFT DIAMETER0.0895 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
SPECIAL FEATURESWEAPON SYSTEM ESSENTIAL
SPECIFICATION/STANDARD DATA81349-MIL-S-20708/78 GOVERNMENT SPECIFICATION
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.).
TRANSFORMATION RATIO0.454 ROTOR TO STATOR NOMINAL
UNDERCUT DIAMETER0.6920 INCHES NOMINAL
UNDERCUT WIDTH0.0620 INCHES NOMINAL
ZRO IMPEDANCE ANGLE IN DEG77.50 MINIMUM AND 80.50 MAXIMUM
ZRO IMPEDANCE MAGNITUDE IN OHMS170.00 MINIMUM AND 215.00 MAXIMUM
ZSS IMPEDANCE ANGLE IN DEG9.00 MINIMUM AND 15.00 MAXIMUM
ZSS IMPEDANCE MAGNITUDE IN OHMS11.00 MINIMUM AND 15.00 MAXIMUM


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