NSN 5990-00-917-4215
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-917-4215 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: 11CT13351, 11CT1335-1, X40301528, X40-301-528, X40301528, X40-301-528, 618380000, 618380-000, 618380, 618380, 11CT4F, 11CT4E001, 11CT4E-001, 11CT4E, 11CT4B, M20708101E, M20708/1-01E, M207081001, M20708/1-001, M207081D001, M20708-1D-001, MILS207081D, MILS20708/1D, MILS207081, MIL-S-20708/1, 11CT4E101E, 11CT4E/1-01E, 11CT4E, 618380, 11CT4E, 3620281, 362028-1, 3620281, 362028-1, M20708101E, M20708/1-01E, AS207081, AS20708/1, 352250005265, 5990-00-917-4215, 00-917-4215, 5990009174215, 009174215
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JUL 27, 1966 | 00-917-4215 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-917-4215
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 11CT1335-1 | 14404 | AMETEK TECHNICAL & INDUSTRIALPRODUCTS, INC. |
| X40-301-528 | S3712 | BAE SYSTEMS BOFORS AB |
| X40-301-528 | S3715 | BOFORS AB |
| 618380-000 | 56232 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| 618380 | 56232 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| 618380 | 02769 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| 11CT4F | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 11CT4E-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 11CT4E | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 11CT4B | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/1-01E | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/1-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708-1D-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MILS20708/1D | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-20708/1 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 11CT4E/1-01E | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 11CT4E | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 618380 | 03956 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS |
| 11CT4E | 97942 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN SYSTEMS |
| 362028-1 | 49956 | RAYTHEON COMPANYDBA RAYTHEON |
| 362028-1 | 3B150 | RAYTHEON COMPANYDBA RAYTHEON |
| M20708/1-01E | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AS20708/1 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| 352250005265 | H0203 | THALES NEDERLANDDBA THALES LAND & JOINT SYSTEMS |
Technical Data | NSN 5990-00-917-4215
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 90.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 18.0 MILLIAMPERES MAXIMUM |
| STATOR INPUT ELECTRICAL POWER RATING | 200.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZSO IMPEDANCE MAGNITUDE IN OHMS | 4350.00 MINIMUM AND 5700.00 MAXIMUM |
| ZSO IMPEDANCE ANGLE IN DEG | 77.30 MINIMUM AND 83.50 MAXIMUM |
| ZRS IMPEDANCE MAGNITUDE IN OHMS | 585.00 MINIMUM AND 700.00 MAXIMUM |
| ZRS IMPEDANCE ANGLE IN DEG | 22.00 MINIMUM AND 32.00 MAXIMUM |
| TRANSFORMATION RATIO | 0.735 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 5.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 10.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 32.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 60.00 |
| 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 NOMINAL |
| 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, STAINLESS |
| 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 1 GOVERNMENT SPECIFICATION |
