NSN 5990-00-902-0764
Part Details | DIFFERENTIAL TRANSMITTER SYNCHRO
5990-00-902-0764 A synchro, the rotor of which is mechanically positioned for modifying electrical angular information, received from a transmitter synchro and transmitting to receiver synchro or control transformer synchro electrical information corresponding to the sum or difference of the electrical input angle and its rotor position angle. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: A15391005, A15391-005, 4351108, 435-1-108, 4351108, 435-1-108, 5990-00-902-0764, 00-902-0764, 5990009020764, 009020764
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | FEB 08, 1967 | 00-902-0764 | 02071 ( SYNCHRO, DIFFERENTIAL TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C

1 Y-ROTOR, 1 Y-STATOR

Cross Reference | NSN 5990-00-902-0764
Part Number | Cage Code | Manufacturer |
---|---|---|
A15391-005 | 12436 | BAE SYSTEMS INFORMATION ANDELECTRONIC SYSTEMS INTEGRATION INC. |
435-1-108 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
435-1-108 | 1K426 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-902-0764
Characteristic | Specifications |
---|---|
BODY SIZE | 15 |
STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
STATOR INPUT CURRENT RATING | 250.0 MILLIAMPERES NOMINAL |
STATOR INPUT ELECTRICAL POWER RATING | 500.0 MILLIWATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ZRO RESISTANCE IN OHMS | 8.30 NOMINAL |
PLUS J ZRO REACTANCE IN OHMS | 45.00 NOMINAL |
ZSO RESISTANCE IN OHMS | 8.00 NOMINAL |
PLUS J ZSO REACTANCE IN OHMS | 40.00 NOMINAL |
ZSS RESISTANCE IN OHMS | 9.50 NOMINAL |
PLUS J ZSS REACTANCE IN OHMS | 5.40 NOMINAL |
ROTOR DC RESISTANCE IN OHMS | 6.20 NOMINAL |
STATOR DC RESISTANCE IN OHMS | 5.90 NOMINAL |
PHASE SHIFT ANGLE IN DEG | 6.700 INPUT TO OUTPUT NOMINAL |
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 30.00 OUTPUT |
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M15.0/P15.0 |
BODY STYLE | STANDARD ROUND C |
SHOULDER DIAMETER | 1.3370 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM |
PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
OVERALL LENGTH | 2.1400 INCHES NOMINAL |
FLANGE DIAMETER | 1.4360 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM |
FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
UNDERCUT DIAMETER | 1.3090 INCHES MINIMUM AND 1.3150 INCHES MAXIMUM |
UNDERCUT WIDTH | 0.0680 INCHES MINIMUM AND 0.0880 INCHES MAXIMUM |
PILOT LENGTH | 0.0400 INCHES NOMINAL |
SHOULDER LENGTH | 0.1320 INCHES NOMINAL |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6000 INCHES NOMINAL |
ALIGNMENT HOLE DEPTH | 0.7500 INCHES NOMINAL |
ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 2.3280 INCHES NOMINAL |
ALIGNMENT HOLE QUANTITY | 4 |
TERMINAL TYPE AND QUANTITY | 6 WIRE LEAD |
TERMINAL LOCATION | REAR |
BODY MATERIAL | STEEL, CORROSION RESISTING |
SPECIAL FEATURES | SHAFT MODIFIED WITH LINEAR DIAL AND KNOB INSTALLATION |
SCHEMATIC DIAGRAM DESIGNATOR | 1 Y-ROTOR, 1 Y-STATOR |