NSN 5990-00-060-2321
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 |