NSN 5990-01-030-5206
Part Details | TRANSMITTER SYNCHRO
5990-01-030-5206 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: VCX316N1, VCX31-6N1, 31CX6A, M20708139001, M20708/139-001, MILS20708139, MIL-S-20708/139, 5990-01-030-5206, 01-030-5206, 5990010305206, 010305206
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | NOV 08, 1976 | 01-030-5206 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-01-030-5206
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| VCX31-6N1 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| 31CX6A | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/139-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-20708/139 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5990-01-030-5206
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 31 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 191.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 2.26 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 60.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 693.00 NOMINAL |
| ZSS RESISTANCE IN OHMS | 63.00 NOMINAL |
| ZRO IMPEDANCE ANGLE IN DEG | 83.20 NOMINAL |
| ZSS IMPEDANCE ANGLE IN DEG | 20.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 53.60 MAXIMUM |
| STATOR DC RESISTANCE IN OHMS | 52.00 NOMINAL |
| TRANSFORMATION RATIO | 0.783 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 4.400 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 10.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 30.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 100.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M8.0/P8.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 0.50 INCH-OUNCES MAXIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 2.7000 INCHES NOMINAL |
| PILOT DIAMETER | 0.2405 INCHES NOMINAL |
| OVERALL LENGTH | 4.1200 INCHES MAXIMUM |
| FLANGE DIAMETER | 3.1000 INCHES NOMINAL |
| FLANGE THICKNESS | 0.2500 INCHES NOMINAL |
| UNDERCUT DIAMETER | 2.7500 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0250 INCHES NOMINAL |
| PILOT LENGTH | 0.3750 INCHES NOMINAL |
| SHOULDER LENGTH | 0.1850 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 3.3800 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM ALLOY |
| 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 139 GOVERNMENT SPECIFICATION |
| FRAGILITY FACTOR | MODERATELY RUGGED |
