NSN 5990-00-852-2363
Part Details | TRANSMITTER SYNCHRO
5990-00-852-2363 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: 23CX6, VCX23366B, VCX23/36-6B, M207085201D, M20708/52-01D, AY240BA 9 A1, 397001024, 397-001-024, 23CX6D, M2070852C001, M20708/52C-001, M207085201D, M20708/52-01D, M2070852001, M20708/52-001, MILS2070852, MIL-S-20708/52, AS2070852, AS20708/52, 5990-00-852-2363, 00-852-2363, 5990008522363, 008522363
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | NOV 25, 1966 | 00-852-2363 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND D
Cross Reference | NSN 5990-00-852-2363
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 23CX6 | 08842 | ABACUS ELECTRONICS CORP |
| VCX23/36-6B | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| M20708/52-01D | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| AY240BA 9 A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 397-001-024 | 07421 | INTERSTATE ELECTRONICS CORPORATIONDBA L-3 INTERSTATE ELECTRONICS |
| 23CX6D | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/52C-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/52-01D | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/52-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-20708/52 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| AS20708/52 | 0VH01 | SAE CUSTOMER SERVICEDEPT 2045 |
Technical Data | NSN 5990-00-852-2363
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 23 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 80.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 1.4 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 60.0 NOMINAL |
| ZRO IMPEDANCE MAGNITUDE IN OHMS | 1450.00 MINIMUM AND 1700.00 MAXIMUM |
| ZRO IMPEDANCE ANGLE IN DEG | 79.00 MINIMUM AND 83.00 MAXIMUM |
| ZSS IMPEDANCE MAGNITUDE IN OHMS | 155.00 MINIMUM AND 310.00 MAXIMUM |
| ZSS IMPEDANCE ANGLE IN DEG | 10.00 MINIMUM AND 15.00 MAXIMUM |
| TRANSFORMATION RATIO | 0.783 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 6.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 20.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 30.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 60.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M6.0/P6.0 |
| TORQUE GRADIENT PER ANGULAR DEG | 0.200 INCH-OUNCES MAXIMUM |
| BODY STYLE | STANDARD ROUND D |
| SHOULDER DIAMETER | 1.9850 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM |
| PILOT DIAMETER | 0.5950 INCHES NOMINAL |
| SECOND SHOULDER DIAMETER | 1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM |
| SECOND SHOULDER LENGTH | 0.1700 INCHES NOMINAL |
| OVERALL LENGTH | 4.2990 INCHES NOMINAL |
| FLANGE DIAMETER | 2.2490 INCHES MINIMUM AND 2.2500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.2500 INCHES NOMINAL |
| BODY DIAMETER | 1.9900 INCHES MAXIMUM |
| PILOT LENGTH | 0.0430 INCHES NOMINAL |
| SHOULDER LENGTH | 0.1500 INCHES NOMINAL |
| AFT OF FIRST FLANGE DIAMETER | 1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 3.5800 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL |
| 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 52 GOVERNMENT SPECIFICATION |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| FRAGILITY FACTOR | MODERATELY RUGGED |
| END ITEM IDENTIFICATION | GUN FIRE CONTROL SYSTEM, MK 68; STRATEGIC WEAPON SYSTEMS (POSEIDON AND TRIDENT); WEATHER RADAR SET AN/FPS-77; 485L TACS; SPRUANCE CLASS DD (963); DEF COMM METEORL (AN/TMQ-028 AN/TCC-76, AN/TPS-068, AN-TCC-77); COMMUNICATIONS TERMINAL SATELLITE AN/GSC-39(V)1; KIDD CLASS DDG; DEFENSE METEREOLOGICAL SATELLITE PROGRAM (DMSP) |
