Part Details | TRANSMITTER SYNCHRO
5990-00-924-4165 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: 11CX13461, 11CX1346-1, 11CX4E2001, 11CX4E/2-001, AS 207082, AS 20708/2, V23401E0001A102, V23401-E0001-A102, 618381000, 618381-000, 618381, 11CX4E, 11CX4C, M20708201E, M20708/2-01E, M207082001, M20708/2-001, M20708&2C001, MILS207082, MIL-S-20708/2, M207082001, M20708/2-001, 26V11CX4E, 26V-11CX4E, 2625497, 45090012712, 450900-1271-2, 4509001271002, 450900-1271-002, AS20708, 352250005264, 069732101, 5990-00-924-4165, 00-924-4165, 5990009244165, 009244165
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 20, 1966 | 00-924-4165 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-924-4165
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 11CX1346-1 | 14404 | AMETEK TECHNICAL & INDUSTRIALPRODUCTS, INC. |
| 11CX4E/2-001 | B6577 | ELCOS BVBA |
| AS 20708/2 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| V23401-E0001-A102 | C0426 | HENSOLDT SENSORS GMBH |
| 618381-000 | 56232 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| 618381 | 56232 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| 11CX4E | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 11CX4C | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/2-01E | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/2-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708&2C001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-20708/2 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/2-001 | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
| 26V-11CX4E | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 2625497 | 53711 | NAVAL SEA SYSTEMS COMMAND |
| 450900-1271-2 | D4856 | NORTHROP GRUMMAN LITEF GMBHDBA LITEF |
| 450900-1271-002 | D4856 | NORTHROP GRUMMAN LITEF GMBHDBA LITEF |
| AS20708 | 0VH01 | SAE CUSTOMER SERVICEDEPT 2045 |
| 352250005264 | H0203 | THALES NEDERLANDDBA THALES LAND & JOINT SYSTEMS |
| 069732101 | D1876 | WAERTSILAE ELAC NAUTIK GMBH |
Technical Data | NSN 5990-00-924-4165
| 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 IMPEDANCE MAGNITUDE IN OHMS | 3720.00 MINIMUM AND 4700.00 MAXIMUM |
| ZRO IMPEDANCE ANGLE IN DEG | 80.00 MINIMUM AND 84.00 MAXIMUM |
| ZSS IMPEDANCE MAGNITUDE IN OHMS | 410.00 MINIMUM AND 500.00 MAXIMUM |
| ZSS IMPEDANCE ANGLE IN DEG | 17.00 MINIMUM AND 26.00 MAXIMUM |
| TRANSFORMATION RATIO | 0.783 STATOR TO ROTOR 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 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 | 2.3560 INCHES NOMINAL |
| 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 | 0.0620 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.7940 INCHES MAXIMUM |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES MINIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8120 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 2 GOVERNMENT SPECIFICATION |
| FRAGILITY FACTOR | MODERATELY RUGGED |