NSN 5990-00-636-4151
Part Details | TRANSMITTER SYNCHRO
5990-00-636-4151 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: TX376E4, TX37-6E4, 5617924, 561792-4, 5HG, VTX376E4, VTX37-6E4, 23401A, 2340-1A, 35639500001, 3563950-0001, 852485, 5HGMK6, 7410366 P001, 139D688, MILS2335, MIL-S-2335, 5HGMK6, SK139518, SK137160, 852485, 5617924, 561792-4, 524059, 213417, 173113, 212818, 494550226, 494550-226, 5990-00-636-4151, 00-636-4151, 5990006364151, 006364151
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-636-4151 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND DOUBLE FLANGE B
Cross Reference | NSN 5990-00-636-4151
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| TX37-6E4 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| 561792-4 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| 5HG | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| VTX37-6E4 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| 2340-1A | 02987 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX FLIGHT SYSTEMS |
| 3563950-0001 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 852485 | 56232 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| 5HGMK6 | 56232 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| 7410366 P001 | 03538 | LOCKHEED MARTIN CORPORATIONDIV RMS |
| 139D688 | 03538 | LOCKHEED MARTIN CORPORATIONDIV RMS |
| MIL-S-2335 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 5HGMK6 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| SK139518 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| SK137160 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 852485 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 561792-4 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 524059 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 213417 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 173113 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 212818 | 53711 | NAVAL SEA SYSTEMS COMMAND |
| 494550-226 | 30086 | SPD ELECTRICAL SYSTEMS, INC |
Technical Data | NSN 5990-00-636-4151
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 5 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 600.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 7.0 WATTS MAXIMUM |
| FREQUENCY IN HERTZ | 60.0 NOMINAL |
| MAXIMUM TEMP RISE | 50.0 DEG CELSIUS |
| TORQUE GRADIENT PER ANGULAR DEG | 0.400 INCH-OUNCES MINIMUM |
| BODY STYLE | STANDARD ROUND DOUBLE FLANGE B |
| SHOULDER DIAMETER | 3.3750 INCHES MAXIMUM |
| PILOT DIAMETER | 1.6300 INCHES MAXIMUM |
| OVERALL LENGTH | 6.3600 INCHES MAXIMUM |
| FLANGE DIAMETER | 3.6230 INCHES MINIMUM AND 3.6250 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.2450 INCHES MINIMUM AND 0.2500 INCHES MAXIMUM |
| DISTANCE BETWEEN FLANGES | 1.8070 INCHES MINIMUM AND 1.8170 INCHES MAXIMUM |
| PILOT LENGTH | 0.1750 INCHES NOMINAL |
| SHOULDER LENGTH | 1.2450 INCHES MINIMUM AND 1.2550 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| SPECIAL FEATURES | ROUND,THREADED,SLOTED SHAFT; SLOT DEPTH 0.050 INCH; SLOT WIDTH 0.035 INCH |
| 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 |
