Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-060-2321 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: VCT236N3, VCT23-6N3, 24536001, 24536-001, 73783611, 737836-11, 73783611, 737836-11, 23CT6D, M207085301D, M20708/53-01D, M2070853001, M20708/53-001, M207085301, M20708-53-01, MILS2070853, MIL-S-20708/53, 23M2E2Q, AS2070853, AS20708/53, 5990-00-060-2321, 00-060-2321, 5990000602321, 000602321
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JUN 13, 1967 | 00-060-2321 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND D
Cross Reference | NSN 5990-00-060-2321
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| VCT23-6N3 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| 24536-001 | 98853 | HAMILTON STANDARD ELECTRONICSSYSTEMS INC |
| 737836-11 | 49671 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| 737836-11 | 02769 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| 23CT6D | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/53-01D | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/53-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708-53-01 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-20708/53 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 23M2E2Q | K0624 | MUIRHEAD AEROSPACE LTDDBA MUIRHEAD AVIONICS |
| AS20708/53 | 0VH01 | SAE CUSTOMER SERVICEDEPT 2045 |
Technical Data | NSN 5990-00-060-2321
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 23 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 90.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 18.5 MILLIAMPERES MAXIMUM |
| STATOR INPUT ELECTRICAL POWER RATING | 400.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 60.0 NOMINAL |
| ZSO IMPEDANCE MAGNITUDE IN OHMS | 4200.00 MINIMUM AND 5100.00 MAXIMUM |
| ZSO IMPEDANCE ANGLE IN DEG | 70.00 MINIMUM AND 76.00 MAXIMUM |
| ZRS IMPEDANCE MAGNITUDE IN OHMS | 1350.00 MINIMUM AND 1650.00 MAXIMUM |
| ZRS IMPEDANCE ANGLE IN DEG | 14.00 MINIMUM AND 20.00 MAXIMUM |
| TRANSFORMATION RATIO | 0.735 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 14.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 10.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 30.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 45.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M6.0/P6.0 |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 0.20 INCH-OUNCES MAXIMUM |
| BODY STYLE | STANDARD ROUND D |
| SHOULDER DIAMETER | 1.9850 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM |
| PILOT DIAMETER | 0.5950 INCHES NOMINAL |
| SECOND SHOULDER DIAMETER | 1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM |
| SECOND SHOULDER LENGTH | 0.1700 INCHES NOMINAL |
| OVERALL LENGTH | 4.2990 INCHES NOMINAL |
| FLANGE DIAMETER | 2.2490 INCHES MINIMUM AND 2.2500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.2500 INCHES NOMINAL |
| BODY DIAMETER | 1.9900 INCHES MAXIMUM |
| PILOT LENGTH | 0.0430 INCHES NOMINAL |
| SHOULDER LENGTH | 0.2500 INCHES NOMINAL |
| AFT OF FIRST FLANGE DIAMETER | 1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 3.5800 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| TEST DATA DOCUMENT | 81349-MIL-S-20708 SPECIFICATION (INCLUDES ENGINEERING TYPE BULLETINS, BROCHURES,ETC., THAT REFLECT SPECIFICATION TYPE DATA IN SPECIFICATION FORMAT; EXCLUDES COMMERCIAL CATALOGS, INDUSTRY DIRECTORIES, AND SIMILAR TRADE PUBLICATIONS, REFLECTING GENERAL TYPE DATA ON CERTAIN ENVIRONMENTAL AND PERFORMANCE REQUIREMENTS AND TEST CONDITIONS THAT ARE SHOWN AS "TYPICAL", "AVERAGE", "NOMINAL", ETC.). |
| SPECIFICATION/STANDARD DATA | 81349-MIL--20708 TO 53 GOVERNMENT SPECIFICATION |
| SHAFT MAXIMUM RADIAL PLAY | 0.0010 INCHES |
| SHAFT RADIAL PLAY TEST POINT | 0.125 INCHES NOMINAL |
| SHAFT END PLAY | 0.0025 INCHES NOMINAL |
| SHAFT MAXIMUM RUNOUT | 0.0008 INCHES |
| FRAGILITY FACTOR | MODERATELY RUGGED |