5990-00-553-6710 SYNCHRO,RECEIVER Index 5990-00-553-6712 SYNCHRO,CONTROL TRANSFORMER

National Stock Number:
5990-00-553-6711

Federal Supply Class:
5990

National Item Identification Number:
005536711

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:
23TX6A10112GENERAL DYNAMICS MOTION CONTROL LLC
23TX6A81349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
82127780U583SAE INTERNATIONAL
SAE-AS20708/940U583SAE INTERNATIONAL
AY240BA12A155972HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS
MIL-S-20708/9481349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
SAE-AS20708?/940U583SAE INTERNATIONAL
VTX23/36-6B10112GENERAL DYNAMICS MOTION CONTROL LLC


Techincal Specification:
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES-8.0 TO 8.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS0.50 INCH-OUNCES MAXIMUM
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS0.20 INCH-OUNCES MAXIMUM
AFT OF FIRST FLANGE DIAMETER1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM
BODY DIAMETER1.9900 INCHES MINIMUM AND 1.9950 INCHES MAXIMUM
BODY MATERIALSTEEL CORROSION RESISTING
BODY STYLESTANDARD ROUND D
BODY SIZE23
FLANGE DIAMETER2.2490 INCHES MINIMUM AND 2.2500 INCHES MAXIMUM
FLANGE THICKNESS0.2490 INCHES MINIMUM AND 0.2500 INCHES MAXIMUM
FREQUENCY IN HERTZ60.0 NOMINAL
LENGTH0.2410 INCHES MINIMUM AND 0.2520 INCHES MAXIMUM SHOULDER
OVERALL LENGTH4.2940 INCHES NOMINAL
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT75.00 OUTPUT
MAXIMUM TEMP RISE65.0 CELSIUS
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT125.00
MOUNTING SURFACE TO TERMINAL END DISTANCE3.4450 INCHES MAXIMUM
PILOT LENGTH0.0360 INCHES MINIMUM AND 0.0460 INCHES MAXIMUM
PILOT DIAMETER0.5900 INCHES MINIMUM AND 0.6000 INCHES MAXIMUM
PLUS J ZRO REACTANCE IN OHMS494.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS79.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS311.00 NOMINAL
PLUS J ZSO-90 REACTANCE IN OHMS90.00 NOMINAL
ROTOR INPUT CURRENT RATING210.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING5.0 WATTS NOMINAL
ROTOR INPUT VOLTAGE RATING IN VOLTS115.0 NOMINAL
SECOND SHOULDER DIAMETER1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM
SECOND SHOULDER LENGTH0.1670 INCHES MINIMUM AND 0.1700 INCHES MAXIMUM
SHOULDER DIAMETER1.9850 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM
SPECIFICATION/STANDARD DATA81349-MIL-S-20708/94 GOVERNMENT SPECIFICATION
ZRO RESISTANCE IN OHMS132.00 NOMINAL
ZRS RESISTANCE IN OHMS249.00 NOMINAL
ZSO RESISTANCE IN OHMS98.00 NOMINAL
ZSO-90 RESISTANCE IN OHMS90.00 NOMINAL
TERMINAL LOCATIONREAR
TERMINAL TYPE AND QUANTITY7 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 DEG0.130 INCH-OUNCES NOMINAL
TRANSFORMATION RATIO0.783 ROTOR TO STATOR NOMINAL


Click here to Register for Free 30-day Trial