NSN 5990-00-881-1031
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-881-1031 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the rotor is dependent upon both the position of the rotor and the electrical input to the stator from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, or variable transformers.
Alternate Parts: 7101900, M2070879001, M20708/79-001, M2070879D001, M20708-79D-001, MILS2070879, MILS20708-79, 26V08CT4C, M207087901C, M20708/79-01C, 26V08CT4C7901C, 26V-08CT4C/79-01C, 138A916001, AS2070879, AS20708/79, M207087901C, M20708/79-01C, AS2070879, AS20708/79, 5990-00-881-1031, 00-881-1031, 5990008811031, 008811031
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | NOV 17, 1967 | 00-881-1031 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-881-1031
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 7101900 | 93322 | GE AVIATION SYSTEMS LLCDBA GE AVIATION |
| M20708/79-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708-79D-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MILS20708-79 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 26V08CT4C | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/79-01C | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 26V-08CT4C/79-01C | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 138A916001 | 03956 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS |
| AS20708/79 | 0VH01 | SAE CUSTOMER SERVICEDEPT 2045 |
| M20708/79-01C | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AS20708/79 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 5990-00-881-1031
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 23.0 MILLIAMPERES MAXIMUM |
| STATOR INPUT ELECTRICAL POWER RATING | 44.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO IMPEDANCE MAGNITUDE IN OHMS | 830.00 MINIMUM AND 940.00 MAXIMUM |
| ZRO IMPEDANCE ANGLE IN DEG | 16.00 MINIMUM AND 20.00 MAXIMUM |
| ZSO IMPEDANCE MAGNITUDE IN OHMS | 444.00 MINIMUM AND 570.00 MAXIMUM |
| ZSO IMPEDANCE ANGLE IN DEG | 76.00 MINIMUM AND 81.00 MAXIMUM |
| TRANSFORMATION RATIO | 2.203 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 8.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 10.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 25.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
| TORQUE GRADIENT PER ANGULAR DEG | 0.040 INCH-OUNCES MAXIMUM |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.5920 INCHES NOMINAL |
| FLANGE DIAMETER | 0.7450 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.6870 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 |
| 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 79 GOVERNMENT SPECIFICATION |
