NSN 5990-00-465-4829
Part Details | TRANSMITTER SYNCHRO
5990-00-465-4829 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: 7101901, MILS2070878, MIL-S-20708/78, 26V08CX4C, 26V-08CX4C, M207087801C, M20708/78-01C, M2070878001, M20708/78-001, M2070878D001, M20708-78D001, 26V08CX4C7801C, 26V-08CX4C/78-01C, 5315001, 531500-1, AS2070878, AS20708/78, 5990-00-465-4829, 00-465-4829, 5990004654829, 004654829
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 19, 1970 | 00-465-4829 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-465-4829
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 7101901 | 93322 | GE AVIATION SYSTEMS LLCDBA GE AVIATION |
| MIL-S-20708/78 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 26V-08CX4C | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/78-01C | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/78-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708-78D001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 26V-08CX4C/78-01C | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 531500-1 | 96214 | RAYTHEON COMPANYDBA RAYTHEON |
| AS20708/78 | 0VH01 | SAE CUSTOMER SERVICEDEPT 2045 |
Technical Data | NSN 5990-00-465-4829
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 153.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 700.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO IMPEDANCE MAGNITUDE IN OHMS | 170.00 MINIMUM AND 215.00 MAXIMUM |
| ZRO IMPEDANCE ANGLE IN DEG | 77.50 MINIMUM AND 80.50 MAXIMUM |
| ZSS IMPEDANCE MAGNITUDE IN OHMS | 11.00 MINIMUM AND 15.00 MAXIMUM |
| ZSS IMPEDANCE ANGLE IN DEG | 9.00 MINIMUM AND 15.00 MAXIMUM |
| TRANSFORMATION RATIO | 0.454 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 8.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 20.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 20.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 0.04 INCH-OUNCES MAXIMUM |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.6050 INCHES NOMINAL |
| FLANGE DIAMETER | 0.7470 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.6920 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2400 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| 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 78 GOVERNMENT SPECIFICATION |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| FRAGILITY FACTOR | MODERATELY RUGGED |
| END ITEM IDENTIFICATION | T-37 SUPPORT EQUIPMENT; T-38 SUPPORT EEQUIPMENT; AIRCRAFT, VIKING S-3B; PROWLER EA-6B AIRCRAFT; P-3 ORION; AVIONICS SHOP TEST SYSTEM; CUSTOMER FOCUS POOL; AIR TRAFFIC CONTROL |