NSN 5990-00-756-2555
Part Details | TRANSMITTER SYNCHRO
5990-00-756-2555 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: CX234X3, CX23-4X3, VCX23364B, VCX23/36-4B, AY240BA 1 A1, 8212801, 23CX4A, MILS2070894, MIL-S-20708/94, MS510822, MS51082-2, 8212801, 5990-00-756-2555, 00-756-2555, 5990007562555, 007562555
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1960 | 00-756-2555 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND D
Cross Reference | NSN 5990-00-756-2555
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CX23-4X3 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| VCX23/36-4B | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| AY240BA 1 A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 8212801 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 23CX4A | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-20708/94 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MS51082-2 | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
| 8212801 | 19200 | US ARMY ARDEC RDECOM |
Technical Data | NSN 5990-00-756-2555
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 23 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 264.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 2.5 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 50.10 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 544.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 33.80 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 246.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 38.50 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 35.50 NOMINAL |
| ZSS RESISTANCE IN OHMS | 19.30 NOMINAL |
| PLUS J ZSS REACTANCE IN OHMS | 16.40 NOMINAL |
| ZSO-90 RESISTANCE IN OHMS | 17.90 NOMINAL |
| PLUS J ZSO-90 REACTANCE IN OHMS | 86.90 NOMINAL |
| TRANSFORMATION RATIO | 0.783 ROTOR TO STATOR NOMINAL |
| MAXIMUM TEMP RISE | 45.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 75.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 100.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M8.0/P8.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 0.50 INCH-OUNCES MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 0.20 INCH-OUNCES MAXIMUM |
| BODY STYLE | STANDARD ROUND D |
| SHOULDER DIAMETER | 1.9900 INCHES NOMINAL |
| PILOT DIAMETER | 0.6000 INCHES NOMINAL |
| SECOND SHOULDER DIAMETER | 1.9995 INCHES NOMINAL |
| SECOND SHOULDER LENGTH | 0.1720 INCHES NOMINAL |
| OVERALL LENGTH | 4.2940 INCHES MAXIMUM |
| FLANGE DIAMETER | 2.2500 INCHES NOMINAL |
| FLANGE THICKNESS | 0.2500 INCHES NOMINAL |
| BODY DIAMETER | 1.9900 INCHES NOMINAL |
| PILOT LENGTH | 0.0460 INCHES NOMINAL |
| SHOULDER LENGTH | 0.2500 INCHES NOMINAL |
| AFT OF FIRST FLANGE DIAMETER | 1.9995 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 3.4450 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 6 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| 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.). |
| SPECIFICATION/STANDARD DATA | 81349-MIL--20708 TO 94 GOVERNMENT SPECIFICATION |
| FRAGILITY FACTOR | MODERATELY RUGGED |