NSN 5990-00-644-0088

Part Details | DIFFERENTIAL TRANSMITTER SYNCHRO

5990-00-644-0088 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: 7HDGMK11, MILS2335, MIL-S-2335, 561794PC4, 213398PC1, SK139480, 5990-00-644-0088, 00-644-0088, 5990006440088, 006440088

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 01, 196300-644-008802071 ( SYNCHRO, DIFFERENTIAL TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND DOUBLE FLANGE A

Cross Reference | NSN 5990-00-644-0088
Part Number Cage Code Manufacturer
7HDGMK1181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-233581349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
561794PC410001NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT
213398PC110001NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT
SK13948010001NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT
Technical Data | NSN 5990-00-644-0088
Characteristic Specifications
BODY SIZE58
STATOR INPUT VOLTAGE RATING IN VOLTS115.0 NOMINAL
STATOR INPUT CURRENT RATING3.5 AMPERES MAXIMUM
STATOR INPUT ELECTRICAL POWER RATING30.0 WATTS MAXIMUM
FREQUENCY IN HERTZ60.0 NOMINAL
ZRO RESISTANCE IN OHMS400.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS660.00 NOMINAL
TRANSFORMATION RATIO0.990 ROTOR TO STATOR NOMINAL
MAXIMUM TEMP RISE50.0 DEG CELSIUS
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM18.0/P18.0
TORQUE GRADIENT PER ANGULAR DEG4.000 INCH-OUNCES MINIMUM
BODY STYLE STANDARD ROUND DOUBLE FLANGE A
SHOULDER DIAMETER4.8740 INCHES MAXIMUM
PILOT DIAMETER1.7500 INCHES MAXIMUM
SECOND SHOULDER DIAMETER5.5000 INCHES MAXIMUM
SECOND SHOULDER LENGTH0.5000 INCHES MAXIMUM
OVERALL LENGTH9.2100 INCHES MAXIMUM
FLANGE DIAMETER5.7480 INCHES MINIMUM AND 5.7500 INCHES MAXIMUM
FLANGE THICKNESS0.2450 INCHES MINIMUM AND 0.2500 INCHES MAXIMUM
BODY DIAMETER5.3750 INCHES MAXIMUM
DISTANCE BETWEEN FLANGES3.2500 INCHES NOMINAL
PILOT LENGTH0.2500 INCHES NOMINAL
SHOULDER LENGTH1.0600 INCHES NOMINAL
AFT OF SECOND FLANGE DIAMETER4.8750 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE6.6180 INCHES NOMINAL
TERMINAL TYPE AND QUANTITY6 SCREW
TERMINAL LOCATION REAR
BODY MATERIAL ALUMINUM
SPECIAL FEATURESSHAFT KEYED WITH NO. 00 WOODRUFF KEYWHITNEY NO. 207
TEST DATA DOCUMENT81349-MIL-S-2335 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--2335 GOVERNMENT SPECIFICATION