Part Details | RECEIVER SYNCHRO
5990-00-948-9245 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: 994529A, 99-4529A, 994529A, 99-4529A, 994529A, 99-4529A, CRH10AS4F205, CRH-10-AS-4/F205, 10TR9489245, 10TR948-9245, 5013650, 5990-00-948-9245, 00-948-9245, 5990009489245, 009489245
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | APR 11, 1966 | 00-948-9245 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-948-9245
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 99-4529A | 93712 | ALLIANT DEFENSE ELECTRONICS SYSTEMSINC DBA LUNDY TECHNICAL CENTER |
| 99-4529A | 75324 | KILGORE FLARES COMPANY LLC |
| 99-4529A | 48ZY0 | MAS COMPONENTS AND COATINGS LLCDIV MAS COMPONENTS & COATINGS, LLC |
| CRH-10-AS-4/F205 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 10TR948-9245 | 2X130 | MOTION DEVICES TECHNOLOGY, INC. |
| 5013650 | 53711 | NAVAL SEA SYSTEMS COMMAND |
Technical Data | NSN 5990-00-948-9245
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 148.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 600.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 27.50 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 174.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 7.70 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 30.50 NOMINAL |
| ZRS RESISTANCE IN OHMS | 47.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 16.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 16.60 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 7.30 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 5.000 INPUT TO OUTPUT NOMINAL |
| RECEIVER ERROR ANGULAR RANGE IN MINUTES | M30.0/P30.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 5400.00 MILLIMETER-MILLIGRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 2700.00 MILLIMETER-MILLIGRAMS MAXIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.6160 INCHES NOMINAL |
| FLANGE DIAMETER | 0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0630 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.8400 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0380 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES MAXIMUM |
| ALIGNMENT HOLE DEPTH | 0.0500 INCHES MAXIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.6780 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 3 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |
| FRAGILITY FACTOR | MODERATELY RUGGED |