NSN 5990-00-103-0525
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-103-0525 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the rotor is dependent upon both the position of the rotor and the electrical input to the stator from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, or variable transformers.
Alternate Parts: CM41034107, CK41034107, CM41034107, HWC8RVF6L554, HWC8TRVF6F024, HWC-8-TRVF-6/F024, 5317061, 531706-1, 5990-00-103-0525, 00-103-0525, 5990001030525, 001030525
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | JUN 12, 1968 | 00-103-0525 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-103-0525
Part Number | Cage Code | Manufacturer |
---|---|---|
CM41034107 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
CK41034107 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
CM41034107 | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
HWC8RVF6L554 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
HWC-8-TRVF-6/F024 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
531706-1 | 96214 | RAYTHEON COMPANYDBA RAYTHEON |
Technical Data | NSN 5990-00-103-0525
Characteristic | Specifications |
---|---|
BODY SIZE | 8 |
STATOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
STATOR INPUT CURRENT RATING | 5.0 MILLIAMPERES NOMINAL |
STATOR INPUT ELECTRICAL POWER RATING | 10.0 MILLIWATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ZRO RESISTANCE IN OHMS | 634.00 NOMINAL |
PLUS J ZRO REACTANCE IN OHMS | 2756.00 NOMINAL |
ZSO RESISTANCE IN OHMS | 446.00 NOMINAL |
PLUS J ZSO REACTANCE IN OHMS | 2464.00 NOMINAL |
ZRS RESISTANCE IN OHMS | 909.00 NOMINAL |
ROTOR DC RESISTANCE IN OHMS | 480.00 NOMINAL |
STATOR DC RESISTANCE IN OHMS | 370.00 NOMINAL |
TRANSFORMATION RATIO | 0.960 ROTOR TO STATOR NOMINAL |
PHASE SHIFT ANGLE IN DEG | 8.800 INPUT TO OUTPUT NOMINAL |
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M5.0/P5.0 |
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.0 CENTIMETER-GRAMS MAXIMUM |
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS MAXIMUM |
BODY STYLE | STANDARD ROUND A |
PILOT DIAMETER | 0.5000 INCHES NOMINAL |
OVERALL LENGTH | 1.9850 INCHES MAXIMUM |
FLANGE DIAMETER | 0.7500 INCHES NOMINAL |
FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
UNDERCUT DIAMETER | 0.6190 INCHES NOMINAL |
UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
PILOT LENGTH | 0.0400 INCHES NOMINAL |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.5000 INCHES MAXIMUM |
TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
TERMINAL LOCATION | REAR |
BODY MATERIAL | ALUMINUM ALLOY |
FRAGILITY FACTOR | MODERATELY RUGGED |