NSN 5990-00-913-5159
Part Details | RECEIVER SYNCHRO
5990-00-913-5159 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: 15TR4A, 15TRX4, 033243, 15TRX4A, M207081901A, M20708/19-01A, M2070819001, M20708/19-001, M2070819E001, M20708-19E001, MILS2070819, MIL-S-20708/19, 15TRX4A, 302B033243, AS2070819, AS20708/19, M207081901A, M20708/19-01A, AS2070819, AS20708/19, 7674777, 5990-00-913-5159, 00-913-5159, 5990009135159, 009135159
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1960 | 00-913-5159 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-913-5159
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 15TR4A | 99479 | BOWMAR, LLC |
| 15TRX4 | 28199 | L3 TECHNOLOGIES, INC.DBA L3 HENSCHEL |
| 033243 | 34228 | L3 TECHNOLOGIES, INC.DBA L3 KEO |
| 15TRX4A | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/19-01A | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/19-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708-19E001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-20708/19 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 15TRX4A | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 302B033243 | 03956 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS |
| AS20708/19 | 05AY8 | SAE INC |
| M20708/19-01A | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AS20708/19 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| 7674777 | 19200 | US ARMY ARDEC RDECOM |
Technical Data | NSN 5990-00-913-5159
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 190.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 2.9 WATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZSS IMPEDANCE MAGNITUDE IN OHMS | 50.00 MINIMUM AND 82.00 MAXIMUM |
| ZSS IMPEDANCE ANGLE IN DEG | 33.00 MINIMUM AND 46.00 MAXIMUM |
| TRANSFORMATION RATIO | 0.783 STATOR TO ROTOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 5.000 INPUT TO OUTPUT MAXIMUM |
| MAXIMUM TEMP RISE | 35.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 50.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 100.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M6.0/P6.0 |
| RECEIVER ERROR ANGULAR RANGE IN MINUTES | M45.0/P45.0 |
| TORQUE GRADIENT PER ANGULAR DEG | 0.030 INCH-OUNCES MINIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM |
| PILOT DIAMETER | 0.8745 INCHES MINIMUM AND 0.8750 INCHES MAXIMUM |
| OVERALL LENGTH | 2.3120 INCHES NOMINAL |
| FLANGE DIAMETER | 1.4320 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 1.3120 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0780 INCHES NOMINAL |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| SHOULDER LENGTH | 0.1320 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.7720 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES MINIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 1.1000 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| 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 19 GOVERNMENT SPECIFICATION |
| FRAGILITY FACTOR | MODERATELY RUGGED |
