NSN 5990-00-501-2641
Part Details | TRANSMITTER SYNCHRO
5990-00-501-2641 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: AY202S1B, 7909648, 790964-8, AY202S1B, 7909648, 790964-8, 40220601, 4022-06-01, 40220601, 4022-06-01, 5990-00-501-2641, 00-501-2641, 5990005012641, 005012641
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-501-2641 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-501-2641
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AY202S1B | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 790964-8 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY202S1B | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 790964-8 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 4022-06-01 | 58880 | MEGGITT (NEW HAMPSHIRE), INC |
| 4022-06-01 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-501-2641
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 225.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 1.2 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 25.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 115.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 9.50 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 3.80 NOMINAL |
| TRANSFORMATION RATIO | 11.800 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 4.500 INPUT TO OUTPUT NOMINAL |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M10.0/P10.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 5.0 CENTIMETER-GRAMS NOMINAL |
| TORQUE GRADIENT PER ANGULAR DEG | 3000.0 MILLIMETER-MILLIGRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 2.4440 INCHES NOMINAL |
| FLANGE DIAMETER | 1.4360 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 | 1.5510 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES MAXIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8750 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |
| SPECIAL FEATURES | REAR SHAFT DIM. 0.4150 IN. NOM LG,0.1195 IN. MIN 0.1200 IN. MAX DIA,0.0210 IN. MIN 0.0310 IN. MAX W BY 0.0210 IN. MIN 0.0310 IN. MAX DEEP SLOT |