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National Stock Number:
5990-00-644-0090
Federal Supply Class:
5990
National Item Identification Number:
006440090
Description:
SYNCHRO,DIFFERENTIAL TRANSMITTER
Detail:
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.
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Manufacturer Information:
| 1HDG | 81349 | MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M | | 1HDGMK13 | 81349 | MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M | | 213422PC1 | 10001 | NAVAIR AND NAVSEA MANAGED ORIGINAL DESIGN ACTIVITY DWG NOT MATERIAL/PARTS SUPPLIER | | 561790-5 | 10001 | NAVAIR AND NAVSEA MANAGED ORIGINAL DESIGN ACTIVITY DWG NOT MATERIAL/PARTS SUPPLIER | | 2136834G001 | 28527 | L3HARRIS TECHNOLOGIES, INC. | | 2136834G1 | 28527 | L3HARRIS TECHNOLOGIES, INC. | | 561790PC5 | 10001 | NAVAIR AND NAVSEA MANAGED ORIGINAL DESIGN ACTIVITY DWG NOT MATERIAL/PARTS SUPPLIER | | 950509 | 10001 | NAVAIR AND NAVSEA MANAGED ORIGINAL DESIGN ACTIVITY DWG NOT MATERIAL/PARTS SUPPLIER | | 950512 | 10001 | NAVAIR AND NAVSEA MANAGED ORIGINAL DESIGN ACTIVITY DWG NOT MATERIAL/PARTS SUPPLIER | | 951184 | 10001 | NAVAIR AND NAVSEA MANAGED ORIGINAL DESIGN ACTIVITY DWG NOT MATERIAL/PARTS SUPPLIER | | SK139537 | 10001 | NAVAIR AND NAVSEA MANAGED ORIGINAL DESIGN ACTIVITY DWG NOT MATERIAL/PARTS SUPPLIER | | MIL-S-2335 | 81349 | MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M | | MILS2335 | 81349 | MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M | | MS1HDGMK13 | 96906 | MILITARY STANDARDS PROMULGATED BY MILITARY DEPARTMENTS UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M | | SK273120 | 10001 | NAVAIR AND NAVSEA MANAGED ORIGINAL DESIGN ACTIVITY DWG NOT MATERIAL/PARTS SUPPLIER | | VTDX22-39-6A | 10112 | GENERAL DYNAMICS MOTION CONTROL LLC |
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Techincal Specification:
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | -18.0 TO 18.0 | | ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8440 INCHES NOMINAL | | ALIGNMENT HOLE DEPTH | 0.1560 INCHES NOMINAL | | ALIGNMENT HOLE QUANTITY | 3 | | BODY DIAMETER | 2.2300 INCHES NOMINAL | | BODY MATERIAL | ALUMINUM | | BODY STYLE | STANDARD ROUND, REAR MOUNTING FLANGE | | BODY SIZE | 23 | | FLANGE DIAMETER | 2.2480 INCHES MINIMUM AND 2.2500 INCHES MAXIMUM | | FLANGE THICKNESS | 0.2500 INCHES NOMINAL | | FRAGILITY FACTOR | MODERATELY RUGGED | | FREQUENCY IN HERTZ | 60.0 NOMINAL | | LENGTH | 0.0550 INCHES NOMINAL SHOULDER | | OVERALL LENGTH | 4.2000 INCHES MAXIMUM | | MAXIMUM TEMP RISE | 50.0 CELSIUS | | PILOT LENGTH | 0.1250 INCHES NOMINAL | | PILOT DIAMETER | 1.0625 INCHES NOMINAL | | SECOND SHOULDER DIAMETER | 1.9500 INCHES NOMINAL | | SECOND SHOULDER FACE TO REAR FLANGE DISTANCE | 0.0450 INCHES NOMINAL | | SECOND SHOULDER LENGTH | 0.0250 INCHES NOMINAL | | SHOULDER DIAMETER | 1.2500 INCHES NOMINAL | | STATOR INPUT ELECTRICAL POWER RATING | 8.0 WATTS NOMINAL | | STATOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL | | STATOR INPUT CURRENT RATING | 300.0 MILLIAMPERES NOMINAL | | TERMINAL LOCATION | REAR | | TERMINAL TYPE AND QUANTITY | 6 SCREW | | TEST DATA DOCUMENT | 81349-MIL-S-22335 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.). | | TORQUE GRADIENT PER ANGULAR DEG | 0.035 INCH-OUNCES MINIMUM | | TRANSFORMATION RATIO | 0.774 ROTOR TO STATOR NOMINAL |
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