Part Details | TRANSMITTER SYNCHRO
5990-00-018-9723 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: VCX156N2, VCX15-6N2, VCX156D2, VCX15-6D2, M2070820001, M20708/20-001, MILS2070820, MILS20708-20, MILS20708, MIL-S20708, MILS2070820C, MIL-S-20708/20C, 15CX6C, 15CX6B, M2070820C001, M20708/20C-001, M207082002C, M20708/20-02C, M207082001C, M20708/20-01C, 15CX6C, 29391981, 2939198-1, 300D717H02, 181450, 1889768PC23, AS2070820, AS20708/20, 15CS6B, AS2070820, AS20708/20, M207082001C, M20708/20-01C, 5990-00-018-9723, 00-018-9723, 5990000189723, 000189723
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | APR 25, 1967 | 00-018-9723 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-018-9723
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| VCX15-6N2 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| VCX15-6D2 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| M20708/20-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MILS20708-20 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S20708 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-20708/20C | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 15CX6C | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 15CX6B | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/20C-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/20-02C | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/20-01C | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 15CX6C | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 2939198-1 | 53711 | NAVAL SEA SYSTEMS COMMAND |
| 300D717H02 | 90099 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDBA NORTHROP GRUMMAN MARINE SYSTEMS |
| 181450 | 21877 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVAL AND MARINE SYSTEMS |
| 1889768PC23 | 03956 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS |
| AS20708/20 | 0VH01 | SAE CUSTOMER SERVICEDEPT 2045 |
| 15CS6B | 03024 | SENIOR OPERATIONS LLCDBA KETEMA AEROSPACE |
| AS20708/20 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| M20708/20-01C | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 5990-00-018-9723
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 22.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 360.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 60.0 NOMINAL |
| ZRO IMPEDANCE MAGNITUDE IN OHMS | 5335.00 MINIMUM AND 6265.00 MAXIMUM |
| ZRO IMPEDANCE ANGLE IN DEG | 80.00 MINIMUM AND 83.00 MAXIMUM |
| ZSS IMPEDANCE MAGNITUDE IN OHMS | 675.00 MINIMUM AND 825.00 MAXIMUM |
| ZSS IMPEDANCE ANGLE IN DEG | 11.00 MINIMUM AND 16.00 MAXIMUM |
| TRANSFORMATION RATIO | 0.783 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 7.000 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 | 90.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M6.0/P6.0 |
| TORQUE GRADIENT PER ANGULAR DEG | 0.050 INCH-OUNCES MAXIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM |
| PILOT DIAMETER | 0.8745 INCHES MINIMUM AND 0.8750 INCHES MAXIMUM |
| OVERALL LENGTH | 3.0630 INCHES NOMINAL |
| FLANGE DIAMETER | 1.4320 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 1.3120 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 | 2.5230 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES MINIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 1.1000 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 5 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 20 GOVERNMENT SPECIFICATION |
| FRAGILITY FACTOR | MODERATELY RUGGED |