NSN 5990-00-251-7822
Part Details | RECEIVER SYNCHRO
5990-00-251-7822 A synchro consisting of a stator and rotor inductively coupled. The rotor is free to turn in accordance with the electrical input from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: 26V11TR4B, 26V-11TR4B, 26V11TR4B, 26V11TR4C, 26V-11TR4C, M20708501C, M20708/5-01C, M207085001, M20708/5-001, M207085C001, M20708-5C001, M207085, M20708-5, MILS207085A, MIL-S-20708/5A, MILS207085, MIL-S-20708/5, 26V11TR4C, 26V-11TR4C, 1359468, AS20708, VTR11184D, VTR11-18-4D, 5990-00-251-7822, 00-251-7822, 5990002517822, 002517822
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JUL 16, 1969 | 00-251-7822 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-251-7822
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 26V-11TR4B | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| 26V11TR4B | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 26V-11TR4C | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/5-01C | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/5-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708-5C001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708-5 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-20708/5A | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-20708/5 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 26V-11TR4C | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 1359468 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| AS20708 | 0VH01 | SAE CUSTOMER SERVICEDEPT 2045 |
| VTR11-18-4D | 10651 | VERNITRON CORP |
Technical Data | NSN 5990-00-251-7822
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 280.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 1.0 WATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZSS IMPEDANCE MAGNITUDE IN OHMS | 3.40 MINIMUM AND 4.20 MAXIMUM |
| ZSS IMPEDANCE ANGLE IN DEG | 17.00 MINIMUM AND 24.00 MAXIMUM |
| TRANSFORMATION RATIO | 0.454 STATOR TO ROTOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 6.000 INPUT TO OUTPUT MAXIMUM |
| MAXIMUM TEMP RISE | 20.0 DEG CELSIUS |
| RECEIVER ERROR ANGULAR RANGE IN MINUTES | M60.0/P60.0 |
| TORQUE GRADIENT PER ANGULAR DEG | 0.008 INCH-OUNCES MINIMUM |
| 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 | 1.8010 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, 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 5 GOVERNMENT SPECIFICATION |
| FRAGILITY FACTOR | MODERATELY RUGGED |