NSN 5990-00-268-9075
Part Details | DIFFERENTIAL TRANSMITTER SYNCHRO
5990-00-268-9075 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: VTDX456A1, VTDX45-6A1, MILS2335TYPE6HDGMK10, MILS2335, MIL-S-2335, 6HDG, 6DG, 561793PC4, 5617934, 561793-4, 213401PC1, 1480240, 5990-00-268-9075, 00-268-9075, 5990002689075, 002689075
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-268-9075 | 02071 ( SYNCHRO, DIFFERENTIAL TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND DOUBLE FLANGE B
Cross Reference | NSN 5990-00-268-9075
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| VTDX45-6A1 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| MILS2335TYPE6HDGMK10 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-2335 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 6HDG | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 6DG | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 561793PC4 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 561793-4 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 213401PC1 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 1480240 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
Technical Data | NSN 5990-00-268-9075
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 45 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 90.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 2.0 AMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 23.0 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 60.0 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 MAXIMUM |
| BODY STYLE | STANDARD ROUND DOUBLE FLANGE B |
| SHOULDER DIAMETER | 4.2500 INCHES MAXIMUM |
| PILOT DIAMETER | 1.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 7.5300 INCHES MAXIMUM |
| FLANGE DIAMETER | 4.5000 INCHES NOMINAL |
| FLANGE THICKNESS | 0.2510 INCHES MINIMUM AND 0.2550 INCHES MAXIMUM |
| DISTANCE BETWEEN FLANGES | 2.2500 INCHES NOMINAL |
| PILOT LENGTH | 0.3130 INCHES NOMINAL |
| SHOULDER LENGTH | 1.1870 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 6 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |
| SPECIAL FEATURES | SHAFT TO BE FITTED WITH NO. 00 WOOD RUFF KEY WHITNEY 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 |
| FRAGILITY FACTOR | MODERATELY RUGGED |