NSN 5990-00-984-7894
Part Details | RECEIVER SYNCHRO
5990-00-984-7894 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: 23TR6A, AY240BA 13 A1, 23TR6A, MILS2070894, MIL-S-20708/94, MILS17245, MIL-S-17245, 4186800025, 4186800-025, 3157215P1, 315-7215P1, 8212781, 23TR6A, 5990-00-984-7894, 00-984-7894, 5990009847894, 009847894
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-984-7894 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND D
Cross Reference | NSN 5990-00-984-7894
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 23TR6A | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| AY240BA 13 A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 23TR6A | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-20708/94 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-17245 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 4186800-025 | 05869 | RAYTHEON COMPANYDBA RAYTHEON |
| 315-7215P1 | 49956 | RAYTHEON COMPANYDBA RAYTHEON |
| 8212781 | 19200 | US ARMY ARDEC RDECOM |
| 23TR6A | 10651 | VERNITRON CORP |
Technical Data | NSN 5990-00-984-7894
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 23 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 210.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 5.0 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 60.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 132.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 494.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 98.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 311.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 249.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 79.00 NOMINAL |
| ZSO-90 RESISTANCE IN OHMS | 94.00 NOMINAL |
| PLUS J ZSO-90 REACTANCE IN OHMS | 113.00 NOMINAL |
| TRANSFORMATION RATIO | 0.783 STATOR TO ROTOR NOMINAL |
| MAXIMUM TEMP RISE | 65.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 75.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 125.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M8.0/P8.0 |
| RECEIVER ERROR ANGULAR RANGE IN MINUTES | M60.0/P60.0 |
| TORQUE GRADIENT PER ANGULAR DEG | 0.130 INCH-OUNCES NOMINAL |
| BODY STYLE | STANDARD ROUND D |
| SHOULDER DIAMETER | 1.9850 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM |
| PILOT DIAMETER | 0.5900 INCHES MINIMUM AND 0.6000 INCHES MAXIMUM |
| SECOND SHOULDER DIAMETER | 1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM |
| SECOND SHOULDER LENGTH | 0.1680 INCHES MINIMUM AND 0.1700 INCHES MAXIMUM |
| OVERALL LENGTH | 4.2940 INCHES MAXIMUM |
| FLANGE DIAMETER | 2.2490 INCHES MINIMUM AND 2.2500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.2480 INCHES MINIMUM AND 0.2500 INCHES MAXIMUM |
| BODY DIAMETER | 1.9850 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM |
| PILOT LENGTH | 0.0360 INCHES MINIMUM AND 0.0460 INCHES MAXIMUM |
| SHOULDER LENGTH | 0.2500 INCHES NOMINAL |
| AFT OF FIRST FLANGE DIAMETER | 1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 3.4450 INCHES MAXIMUM |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 1.6420 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 3 |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| 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 94 GOVERNMENT SPECIFICATION |
| FRAGILITY FACTOR | MODERATELY RUGGED |
