NSN 5990-00-229-4647

Part Details | DIFFERENTIAL TRANSMITTER SYNCHRO

5990-00-229-4647 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: 26V11CDX4C, 1599016809Z, 26V11CDX4, 26V11CDX4C, 26V-11CDX4C, M207089C001, M20708/9C-001, M20708901C, M20708/9-01C, M207089001, M20708/9-001, MILS207089, MIL-S-20708/9, 26V11CDX4C, 26V-11CDX4C, 26V11CDX4C, 26V-11CDX4C, AS207089, AS20708/9, AS20708901C, AS20708/9-01C, AS207089, AS20708/9, AS20708901C, AS20708/9-01C, 5990-00-229-4647, 00-229-4647, 5990002294647, 002294647

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59FEB 17, 196900-229-464702071 ( SYNCHRO, DIFFERENTIAL TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

SYNCHRO,DIFFERENTIA | 5990-00-229-4647, 002294647
Cross Reference | NSN 5990-00-229-4647
Part Number Cage Code Manufacturer
26V11CDX4C09301KEARFOTT CORP SOMA FORWARDING DIV
1599016809ZA0810LEONARDO S.P.A. - AIRBORNE & SPACESYSTEM DIVISION
26V11CDX481349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
26V-11CDX4C81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/9C-00181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/9-01C81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/9-00181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-20708/981349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
26V-11CDX4C99932MOOG INC.DBA MOOG COMPONENTS GROUP
26V-11CDX4C4H618MOOG INC.DBA MOOG COMPONENTS GROUP
AS20708/90VH01SAE CUSTOMER SERVICEDEPT 2045
AS20708/9-01C0VH01SAE CUSTOMER SERVICEDEPT 2045
AS20708/981343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AS20708/9-01C81343SOCIETY OF AUTOMOTIVE ENGINEERS INC
Technical Data | NSN 5990-00-229-4647
Characteristic Specifications
BODY SIZE11
STATOR INPUT VOLTAGE RATING IN VOLTS11.8 NOMINAL
STATOR INPUT CURRENT RATING150.0 MILLIAMPERES MAXIMUM
STATOR INPUT ELECTRICAL POWER RATING250.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZSO IMPEDANCE MAGNITUDE IN OHMS68.00 MINIMUM AND 85.00 MAXIMUM
ZSO IMPEDANCE ANGLE IN DEG77.00 MINIMUM AND 82.00 MAXIMUM
ZRS IMPEDANCE MAGNITUDE IN OHMS20.00 MINIMUM AND 26.00 MAXIMUM
ZRS IMPEDANCE ANGLE IN DEG22.00 MINIMUM AND 30.00 MAXIMUM
TRANSFORMATION RATIO1.154 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG6.000 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE10.0 DEG CELSIUS
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT17.00 OUTPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT26.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM7.0/P7.0
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS0.07 INCH-OUNCES MAXIMUM
BODY STYLE STANDARD ROUND C
SHOULDER DIAMETER0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM
PILOT DIAMETER0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM
OVERALL LENGTH2.4130 INCHES NOMINAL
FLANGE DIAMETER1.0570 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM
FLANGE THICKNESS0.0930 INCHES NOMINAL
UNDERCUT DIAMETER0.9750 INCHES NOMINAL
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0620 INCHES NOMINAL
SHOULDER LENGTH0.0620 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.8510 INCHES NOMINAL
ALIGNMENT HOLE DEPTH0.1250 INCHES NOMINAL
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.8120 INCHES NOMINAL
ALIGNMENT HOLE QUANTITY4
TERMINAL TYPE AND QUANTITY6 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 9 GOVERNMENT SPECIFICATION
FRAGILITY FACTOR MODERATELY RUGGED