NSN 5990-01-054-4255
Part Details | TRANSMITTER SYNCHRO
5990-01-054-4255 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: VCDX156N3, VCDX15-6N3, 15CDX6C, M207082202C, M20708/22-02C, MILS2070822, MIL-S-20708/22, 5990-01-054-4255, 01-054-4255, 5990010544255, 010544255
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | JAN 20, 1978 | 01-054-4255 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B

Cross Reference | NSN 5990-01-054-4255
Part Number | Cage Code | Manufacturer |
---|---|---|
VCDX15-6N3 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
15CDX6C | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
M20708/22-02C | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
MIL-S-20708/22 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5990-01-054-4255
Characteristic | Specifications |
---|---|
BODY SIZE | 15 |
ROTOR INPUT VOLTAGE RATING IN VOLTS | 90.0 NOMINAL |
ROTOR INPUT CURRENT RATING | 38.0 MILLIAMPERES NOMINAL |
ROTOR INPUT ELECTRICAL POWER RATING | 500.0 MILLIWATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ZSO RESISTANCE IN OHMS | 2050.00 MINIMUM AND 2600.00 MAXIMUM |
PLUS J ZSO REACTANCE IN OHMS | 77.00 MINIMUM AND 83.00 MAXIMUM |
ZRS RESISTANCE IN OHMS | 900.00 MINIMUM AND 1200.00 MAXIMUM |
ZSO-90 RESISTANCE IN OHMS | 2050.00 MINIMUM AND 2600.00 MAXIMUM |
TRANSFORMATION RATIO | 1.154 ROTOR TO STATOR NOMINAL |
PHASE SHIFT ANGLE IN DEG | 9.000 INPUT TO OUTPUT NOMINAL |
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 60.00 INPUT |
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 100.00 |
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 20.00 INCH-OUNCES NOMINAL |
BODY STYLE | STANDARD ROUND B |
SHOULDER DIAMETER | 1.3120 INCHES NOMINAL |
PILOT DIAMETER | 0.8750 INCHES NOMINAL |
OVERALL LENGTH | 3.2170 INCHES MAXIMUM |
FLANGE DIAMETER | 1.4370 INCHES NOMINAL |
FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
UNDERCUT WIDTH | 0.0780 INCHES NOMINAL |
PILOT LENGTH | 0.0400 INCHES NOMINAL |
SHOULDER LENGTH | 0.1320 INCHES NOMINAL |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 2.6770 INCHES MAXIMUM |
TERMINAL TYPE AND QUANTITY | 5 SCREW |
TERMINAL LOCATION | REAR |
BODY MATERIAL | ALUMINUM ALLOY |
TEST DATA DOCUMENT | 81349-MILS20708 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 DATA | 81349-MIL--20708 TO 22 GOVERNMENT SPECIFICATION |
FRAGILITY FACTOR | MODERATELY RUGGED |