NSN 5990-00-644-0102

Part Details | DIFFERENTIAL TRANSMITTER SYNCHRO

5990-00-644-0102 A synchro, the rotor of which is mechanically positioned for modifying electrical angular information, received from a transmitter synchro and transmitting to receiver synchro or control transformer synchro electrical information corresponding to the sum or difference of the electrical input angle and its rotor position angle. Does not include variable resistors, goniometers, variable transformers, or items with dials.

Alternate Parts: 23CDX6A, MILS2070894, MIL-S-20708/94, 8212786, 5990-00-644-0102, 00-644-0102, 5990006440102, 006440102

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 01, 196300-644-010202071 ( SYNCHRO, DIFFERENTIAL TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND D

Cross Reference | NSN 5990-00-644-0102
Part Number Cage Code Manufacturer
23CDX6A81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-20708/9481349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
821278681349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
Technical Data | NSN 5990-00-644-0102
Characteristic Specifications
BODY SIZE23
STATOR INPUT VOLTAGE RATING IN VOLTS90.0 NOMINAL
STATOR INPUT CURRENT RATING112.0 MILLIAMPERES NOMINAL
STATOR INPUT ELECTRICAL POWER RATING2.2 WATTS NOMINAL
FREQUENCY IN HERTZ60.0 NOMINAL
ZRO RESISTANCE IN OHMS330.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS1006.00 NOMINAL
ZSO RESISTANCE IN OHMS211.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS757.00 NOMINAL
ZRS RESISTANCE IN OHMS471.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS127.00 NOMINAL
TRANSFORMATION RATIO1.154 ROTOR TO STATOR NOMINAL
MAXIMUM TEMP RISE45.0 DEG CELSIUS
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT75.00 OUTPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT100.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM8.0/P8.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS0.50 INCH-OUNCES MAXIMUM
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS0.20 INCH-OUNCES MAXIMUM
BODY STYLE STANDARD ROUND D
SHOULDER DIAMETER1.9850 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM
PILOT DIAMETER0.5900 INCHES MINIMUM AND 0.6000 INCHES MAXIMUM
SECOND SHOULDER DIAMETER1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM
SECOND SHOULDER LENGTH0.1680 INCHES MINIMUM AND 0.1700 INCHES MAXIMUM
OVERALL LENGTH4.5440 INCHES MAXIMUM
FLANGE DIAMETER2.2490 INCHES MINIMUM AND 2.2500 INCHES MAXIMUM
FLANGE THICKNESS0.2500 INCHES NOMINAL
BODY DIAMETER1.9850 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM
PILOT LENGTH0.0360 INCHES MINIMUM AND 0.0460 INCHES MAXIMUM
SHOULDER LENGTH0.2460 INCHES MINIMUM AND 0.2520 INCHES MAXIMUM
AFT OF FIRST FLANGE DIAMETER1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM
MOUNTING SURFACE TO TERMINAL END DISTANCE3.4450 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY7 SCREW
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, STAINLESS
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.).
SPECIFICATION/STANDARD DATA81349-MIL--20708 TO 94 GOVERNMENT SPECIFICATION