5990-00-503-4125 SYNCHRO,TRANSMITTER Index 5990-00-503-4127 SYNCHRO,RECEIVER

National Stock Number:
5990-00-503-4126

Federal Supply Class:
5990

National Item Identification Number:
005034126

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:
113F2A95542NORTHROP GRUMMAN SYSTEMS CORPORATION
113F2AC1834KONTRON AG
23TX40U583SAE INTERNATIONAL
23TX481343SOCIETY OF AUTOMOTIVE ENGINEERS INC
23TX481349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
3563240-050396774HONEYWELL INTERNATIONAL INC.
591C27-394033CARDWELL CONDENSER CORP LAPOINTE-ADMIRAL DIV
767481819200US ARMY ARDEC RDECOM
AS20708/940U583SAE INTERNATIONAL
AS20708/9481343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AY240AA 4 A155972HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS
AY240AA 4 A196774HONEYWELL INTERNATIONAL INC.
C737834-149671LOCKHEED MARTIN CORP LOCKHEED MARTIN INFORMATION SYSTEMS AUTOMATED SPARES
MILS1689281349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
MILS2070881349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
VTX23/36-4A10112GENERAL DYNAMICS MOTION CONTROL LLC


Techincal Specification:
ROTOR INPUT VOLTAGE RATING IN VOLTS115.0 NOMINAL
ROTOR INPUT CURRENT RATING1.21 AMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING0.36 WATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
TERMINAL TYPE AND QUANTITY5 SCREW
BODY SIZE23
BODY MATERIALSTEEL CORROSION RESISTING
ZRO IMPEDANCE MAGNITUDE IN OHMS105.00 NOMINAL
ZRO IMPEDANCE ANGLE IN DEG86.00 NOMINAL
TRANSFORMATION RATIO0.783 ROTOR TO STATOR NOMINAL
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES-8.0 TO 8.0
TORQUE GRADIENT PER ANGULAR DEG0.130 INCH-OUNCES NOMINAL
BODY STYLESTANDARD ROUND D
SHOULDER DIAMETER1.9950 INCHES NOMINAL
PILOT DIAMETER0.6000 INCHES NOMINAL
SECOND SHOULDER DIAMETER1.9995 INCHES NOMINAL
SECOND SHOULDER LENGTH0.1540 INCHES NOMINAL
OVERALL LENGTH4.2990 INCHES NOMINAL
FLANGE DIAMETER2.2500 INCHES NOMINAL
FLANGE THICKNESS0.2500 INCHES NOMINAL
BODY DIAMETER1.9840 INCHES NOMINAL
PILOT LENGTH0.0430 INCHES NOMINAL
SHOULDER LENGTH0.2660 INCHES NOMINAL
AFT OF FIRST FLANGE DIAMETER1.9950 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE3.5800 INCHES NOMINAL
SHAFT TYPEROUND, SLOTTED SINGLE SHAFT
SHAFT DIAMETER0.2405 INCHES NOMINAL SINGLE SHAFT
SHAFT LENGTH0.3430 INCHES NOMINAL SINGLE SHAFT
SHAFT THREAD LENGTH0.2670 INCHES NOMINAL SINGLE SHAFT
SHAFT SLOT DEPTH0.0310 INCHES NOMINAL SINGLE SHAFT
SHAFT SLOT WIDTH0.0250 INCHES NOMINAL SINGLE SHAFT
SHAFT THREAD SERIES DESIGNATORUNF SINGLE SHAFT
SHAFT NOMINAL THREAD SIZE0.250 INCHES SINGLE SHAFT
SHAFT THREAD CLASS2A SINGLE SHAFT
SHAFT THREAD DIRECTIONRIGHT-HAND SINGLE SHAFT
TERMINAL LOCATIONREAR
TEST DATA DOCUMENT81349-MIL-S-16892 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.).
FRAGILITY FACTORMODERATELY RUGGED


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