NSN 5990-00-236-8152
Part Details | TRANSMITTER SYNCHRO
5990-00-236-8152 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: AY080AC49A1, 35630800039, 3563080-0039, 22770210001, 2277021-0001, AY080AC49A1, 35630800039, 3563080-0039, 22770210001, 2277021-0001, 5990-00-236-8152, 00-236-8152, 5990002368152, 002368152
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | MAR 10, 1971 | 00-236-8152 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-236-8152
Part Number | Cage Code | Manufacturer |
---|---|---|
AY080AC49A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
3563080-0039 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
2277021-0001 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
AY080AC49A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
3563080-0039 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
2277021-0001 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-236-8152
Characteristic | Specifications |
---|---|
BODY SIZE | 8 |
ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
ROTOR INPUT CURRENT RATING | 29.0 MILLIAMPERES NOMINAL |
ROTOR INPUT ELECTRICAL POWER RATING | 740.0 MILLIWATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ZRO RESISTANCE IN OHMS | 874.00 NOMINAL |
PLUS J ZRO REACTANCE IN OHMS | 3860.00 NOMINAL |
ZSO RESISTANCE IN OHMS | 9.50 NOMINAL |
PLUS J ZSO REACTANCE IN OHMS | 34.00 NOMINAL |
ZRS RESISTANCE IN OHMS | 1480.00 NOMINAL |
PLUS J ZRS REACTANCE IN OHMS | 325.00 NOMINAL |
ROTOR DC RESISTANCE IN OHMS | 687.00 NOMINAL |
STATOR DC RESISTANCE IN OHMS | 10.30 NOMINAL |
PHASE SHIFT ANGLE IN DEG | 9.200 INPUT TO OUTPUT NOMINAL |
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 75.00 |
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 7.0 CENTIMETER-GRAMS NOMINAL |
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 MILLIMETER-MILLIGRAMS NOMINAL |
TORQUE GRADIENT PER ANGULAR DEG | 2400.000 MILLIMETER-MILLIGRAMS NOMINAL |
BODY STYLE | STANDARD ROUND A |
PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
OVERALL LENGTH | 1.6150 INCHES NOMINAL |
FLANGE DIAMETER | 0.7490 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
FLANGE THICKNESS | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
UNDERCUT DIAMETER | 0.6880 INCHES MINIMUM AND 0.6910 INCHES MAXIMUM |
UNDERCUT WIDTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
PILOT LENGTH | 0.0390 INCHES MINIMUM AND 0.0430 INCHES MAXIMUM |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2400 INCHES MAXIMUM |
ALIGNMENT HOLE DEPTH | 0.0500 INCHES NOMINAL |
ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.5670 INCHES MINIMUM AND 0.5730 INCHES MAXIMUM |
ALIGNMENT HOLE QUANTITY | 2 |
TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
TERMINAL LOCATION | REAR |
BODY MATERIAL | STEEL, STAINLESS |
SHAFT MAXIMUM RADIAL PLAY | 0.0005 INCHES |
SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
SHAFT END PLAY | 0.0003 INCHES MINIMUM AND 0.0008 INCHES MAXIMUM |
SHAFT END PLAY DETERMINING WEIGHT | 8.0 OUNCES |
SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
FRAGILITY FACTOR | MODERATELY RUGGED |