NSN 5990-00-644-0088
Part Details | DIFFERENTIAL TRANSMITTER SYNCHRO
5990-00-644-0088 A synchro, the rotor of which is mechanically positioned for modifying electrical angular information, received from a transmitter synchro and transmitting to receiver synchro or control transformer synchro electrical information corresponding to the sum or difference of the electrical input angle and its rotor position angle. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: MILS2335, MIL-S-2335, 7HDGMK11, SK139480, 561794PC4, 213398PC1, 5990-00-644-0088, 00-644-0088, 5990006440088, 006440088
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-644-0088 | 02071 ( SYNCHRO, DIFFERENTIAL TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND DOUBLE FLANGE A
Cross Reference | NSN 5990-00-644-0088
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| MIL-S-2335 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 7HDGMK11 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| SK139480 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 561794PC4 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 213398PC1 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
Technical Data | NSN 5990-00-644-0088
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 58 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 3.5 AMPERES MAXIMUM |
| STATOR INPUT ELECTRICAL POWER RATING | 30.0 WATTS MAXIMUM |
| FREQUENCY IN HERTZ | 60.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 400.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 660.00 NOMINAL |
| TRANSFORMATION RATIO | 0.990 ROTOR TO STATOR NOMINAL |
| MAXIMUM TEMP RISE | 50.0 DEG CELSIUS |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M18.0/P18.0 |
| TORQUE GRADIENT PER ANGULAR DEG | 4.000 INCH-OUNCES MINIMUM |
| BODY STYLE | STANDARD ROUND DOUBLE FLANGE A |
| SHOULDER DIAMETER | 4.8740 INCHES MAXIMUM |
| PILOT DIAMETER | 1.7500 INCHES MAXIMUM |
| SECOND SHOULDER DIAMETER | 5.5000 INCHES MAXIMUM |
| SECOND SHOULDER LENGTH | 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 9.2100 INCHES MAXIMUM |
| FLANGE DIAMETER | 5.7480 INCHES MINIMUM AND 5.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.2450 INCHES MINIMUM AND 0.2500 INCHES MAXIMUM |
| BODY DIAMETER | 5.3750 INCHES MAXIMUM |
| DISTANCE BETWEEN FLANGES | 3.2500 INCHES NOMINAL |
| PILOT LENGTH | 0.2500 INCHES NOMINAL |
| SHOULDER LENGTH | 1.0600 INCHES NOMINAL |
| AFT OF SECOND FLANGE DIAMETER | 4.8750 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 6.6180 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 6 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |
| SPECIAL FEATURES | SHAFT KEYED WITH NO. 00 WOODRUFF KEYWHITNEY NO. 207 |
| TEST DATA DOCUMENT | 81349-MIL-S-2335 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--2335 GOVERNMENT SPECIFICATION |