NSN 5990-00-822-5451
Part Details | RECEIVER SYNCHRO
5990-00-822-5451 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: VTR23364B, VTR23/36-4B, 3157215P2, 315-7215P2, 23TR4A, MILS2070894, MILS20708-94, MS510823, MS51082-3, 23TR4A, AS2070894, AS20708/94, 5990-00-822-5451, 00-822-5451, 5990008225451, 008225451
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1962 | 00-822-5451 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND D
Cross Reference | NSN 5990-00-822-5451
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| VTR23/36-4B | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| 315-7215P2 | 52315 | KLEIN MARINE SYSTEMS, INC. |
| 23TR4A | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MILS20708-94 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MS51082-3 | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
| 23TR4A | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AS20708/94 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 5990-00-822-5451
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 23 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 945.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 7.8 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 9.10 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 119.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 8.20 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 61.50 NOMINAL |
| ZRS RESISTANCE IN OHMS | 12.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 9.62 NOMINAL |
| ZSO-90 RESISTANCE IN OHMS | 6.16 NOMINAL |
| PLUS J ZSO-90 REACTANCE IN OHMS | 6.16 NOMINAL |
| TRANSFORMATION RATIO | 0.783 ROTOR TO STATOR 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 | 100.00 |
| 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 | 0.5990 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 | 6 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| SPECIAL FEATURES | DEGAUSSING EQUIPMENT |
| 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 |
| NONDEFINITIVE SPEC/STD DATA | 23TRA4A TYPE |
| CRITICALITY CODE JUSTIFICATION | FEAT |
