Part Details | TRANSMITTER SYNCHRO
5990-00-206-3753 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.
Alternate Parts: VCX114G1, VCX11-4G1, 011702M1, 011-702M1, 11CX4E, 011702M1, 011-702M1, M207082C005, M20708/2C-005, M20708205E, M20708/2-05E, M207082005, M20708/2-005, MILS207082, MIL-S-20708/2, 11CX4E, 11CX4E, 1.791521, 59 00013, 59 000-13, AS207082, AS20708/2, 5990-00-206-3753, 00-206-3753, 5990002063753, 002063753
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | APR 13, 1973 | 00-206-3753 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-206-3753
Part Number | Cage Code | Manufacturer |
---|---|---|
VCX11-4G1 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
011-702M1 | 99743 | IMC MAGNETICS CORPWESTERN DIV |
11CX4E | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
011-702M1 | 92703 | KEMTRON ELECTRON PRODUCTS INC |
M20708/2C-005 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
M20708/2-05E | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
M20708/2-005 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
MIL-S-20708/2 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
11CX4E | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
11CX4E | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
1.791521 | D2865 | RAYTHEON ANSCHUETZ GMBHDBA RAYTHEON ELECTRICS GMBH |
59 000-13 | D9853 | ROCKWELL COLLINS DEUTSCHLANDSERVICES GMBH |
AS20708/2 | 0VH01 | SAE CUSTOMER SERVICEDEPT 2045 |
Technical Data | NSN 5990-00-206-3753
Characteristic | Specifications |
---|---|
BODY SIZE | 11 |
ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
ROTOR INPUT CURRENT RATING | 31.0 MILLIAMPERES MAXIMUM |
ROTOR INPUT ELECTRICAL POWER RATING | 490.0 MILLIWATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ZRO RESISTANCE IN OHMS | 3720.00 MINIMUM AND 4700.00 MAXIMUM |
ZSS RESISTANCE IN OHMS | 410.00 MINIMUM AND 500.00 MAXIMUM |
ZRO IMPEDANCE MAGNITUDE IN OHMS | 80.00 MINIMUM AND 84.00 MAXIMUM |
ZSS IMPEDANCE MAGNITUDE IN OHMS | 17.00 MINIMUM AND 26.00 MAXIMUM |
TRANSFORMATION RATIO | 0.783 ROTOR TO STATOR NOMINAL |
PHASE SHIFT ANGLE IN DEG | 4.500 INPUT TO OUTPUT NOMINAL |
MAXIMUM TEMP RISE | 20.0 DEG CELSIUS |
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 45.00 OUTPUT |
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 75.00 |
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 0.07 INCH-OUNCES MAXIMUM |
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 0.07 INCH-OUNCES MAXIMUM |
BODY STYLE | STANDARD ROUND C |
SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM |
OVERALL LENGTH | 2.3360 INCHES MINIMUM AND 2.3760 INCHES MAXIMUM |
FLANGE DIAMETER | 1.0570 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
UNDERCUT DIAMETER | 0.9750 INCHES NOMINAL |
UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
PILOT LENGTH | 0.0450 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
SHOULDER LENGTH | 0.0590 INCHES MINIMUM AND 0.0790 INCHES MAXIMUM |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.7910 INCHES MINIMUM AND 1.8110 INCHES MAXIMUM |
ALIGNMENT HOLE DEPTH | 0.1250 INCHES NOMINAL |
ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.6250 INCHES NOMINAL |
SECURING HOLE QUANTITY | 4 |
MOUNTING FACILITY SCREW THREAD SERIES DESIGNATOR | UNC |
MOUNTING FACILITY NOMINAL SCREW THREAD DIAMETER | 0.112 INCHES |
TERMINAL TYPE AND QUANTITY | 5 SCREW |
TERMINAL LOCATION | REAR |
BODY MATERIAL | STEEL, STAINLESS |
TEST DATA DOCUMENT | 81349-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.). |
FRAGILITY FACTOR | MODERATELY RUGGED |