NSN 5990-00-978-4936
Part Details | TRANSMITTER SYNCHRO
5990-00-978-4936 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: 11TX336G3, 11TX-336-G-3, 11TX4C, 11TX4C001, 11TX4C, M20708401C, M20708/4-01C, M207084C001, M20708-4C001, M207084001, M20708-4-001, MILS207084C, MILS20708-4C, MILS207084, MIL-S-20708/4, M207084001, M20708/4-001, 5990-00-978-4936, 00-978-4936, 5990009784936, 009784936
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | OCT 12, 1966 | 00-978-4936 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-978-4936
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 11TX-336-G-3 | 06989 | API HAROWE INCDBA API MOTION DIV API |
| 11TX4C | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
| 11TX4C001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 11TX4C | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/4-01C | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708-4C001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708-4-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MILS20708-4C | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-20708/4 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/4-001 | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
Technical Data | NSN 5990-00-978-4936
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 60.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 1.0 WATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZSS IMPEDANCE MAGNITUDE IN OHMS | 180.00 MINIMUM AND 250.00 MAXIMUM |
| ZSS IMPEDANCE ANGLE IN DEG | 20.00 MINIMUM AND 28.00 MAXIMUM |
| TRANSFORMATION RATIO | 0.783 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 6.000 INPUT TO OUTPUT MAXIMUM |
| MAXIMUM TEMP RISE | 25.0 DEG CELSIUS |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
| TORQUE GRADIENT PER ANGULAR DEG | 0.070 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 NOMINAL |
| 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.). |
