NSN 5990-00-099-0699

Part Details | CONTROL TRANSFORMER SYNCHRO


5990-00-099-0699 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the rotor is dependent upon both the position of the rotor and the electrical input to the stator from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, or variable transformers.

Alternate Parts: 8CT380D68M, 26V08CT4C, 26V-08CT4C, 26V08CT4C, 26V-08CT4C, M207087902C, M20708/79-02C, M2070879002, M20708/79-002, MILS2070879, MIL-S-20708/79, MS2070879D002, MS20708-79D002, 26V08CT4C7902C, 26V-08CT4C/79-02C, 26V08CT4C, 26V-08CT4C, AS2070879, AS20708/79, 5990-00-099-0699, 00-099-0699, 5990000990699, 000990699

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59DEC 13, 197200-099-069915289 ( SYNCHRO, CONTROL TRANSFORMER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND A


Cross Reference | NSN 5990-00-099-0699
Part Number Cage Code Manufacturer
8CT380D68M06989API HAROWE INCDBA API MOTION DIV API
26V-08CT4C88818KEARFOTT CORPORATIONDBA KEARFOTT
26V-08CT4C81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/79-02C81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/79-00281349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-20708/7981349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MS20708-79D00296906MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS
26V-08CT4C/79-02C99932MOOG INC.DBA MOOG COMPONENTS GROUP
26V-08CT4C99932MOOG INC.DBA MOOG COMPONENTS GROUP
AS20708/790VH01SAE CUSTOMER SERVICEDEPT 2045

Technical Data | NSN 5990-00-099-0699
Characteristic Specifications
BODY SIZE8
STATOR INPUT VOLTAGE RATING IN VOLTS10.2 NOMINAL
STATOR INPUT CURRENT RATING23.0 MILLIAMPERES NOMINAL
STATOR INPUT ELECTRICAL POWER RATING0.053 WATTS MAXIMUM
FREQUENCY IN HERTZ400.0 NOMINAL
ZSO IMPEDANCE MAGNITUDE IN OHMS444.00 MINIMUM AND 70.00 MAXIMUM
ZSO IMPEDANCE ANGLE IN DEG76.00 MINIMUM AND 81.00 MAXIMUM
ZRS IMPEDANCE MAGNITUDE IN OHMS830.00 MINIMUM AND 940.00 MAXIMUM
ZRS IMPEDANCE ANGLE IN DEG16.00 MINIMUM AND 20.00 MAXIMUM
TRANSFORMATION RATIO2.203 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG8.000 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE10.0 DEG CELSIUS
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT25.00 OUTPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT30.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM7.0/P7.0
TORQUE GRADIENT PER ANGULAR DEG0.040 INCH-OUNCES MAXIMUM
BODY STYLE STANDARD ROUND A
PILOT DIAMETER0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM
OVERALL LENGTH1.6150 INCHES NOMINAL
FLANGE DIAMETER0.7450 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM
FLANGE THICKNESS0.0620 INCHES NOMINAL
UNDERCUT DIAMETER0.6870 INCHES NOMINAL
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0620 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2400 INCHES NOMINAL
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
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 79 GOVERNMENT SPECIFICATION
FRAGILITY FACTOR MODERATELY RUGGED