NSN 5990-00-636-4111
Part Details | RECEIVER SYNCHRO
5990-00-636-4111 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: VTR23364A, VTR23/36-4A, C7378342, C737834-2, 23TR4, MILS2070894, MILS20708-94, 4670011, 467001-1, 23TR4, AS2070894, AS20708/94, 23TR4, 7674819, 5990-00-636-4111, 00-636-4111, 5990006364111, 006364111
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | JAN 01, 1963 | 00-636-4111 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND D
Cross Reference | NSN 5990-00-636-4111
Part Number | Cage Code | Manufacturer |
---|---|---|
VTR23/36-4A | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
C737834-2 | 49671 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
23TR4 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
MILS20708-94 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
467001-1 | 95542 | NORTHROP GRUMMAN SYSTEMS CORPORATION |
23TR4 | 95542 | NORTHROP GRUMMAN SYSTEMS CORPORATION |
AS20708/94 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
23TR4 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
7674819 | 19200 | US ARMY ARDEC RDECOM |
Technical Data | NSN 5990-00-636-4111
Characteristic | Specifications |
---|---|
BODY SIZE | 23 |
ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
ROTOR INPUT CURRENT RATING | 945.0 MILLIAMPERES NOMINAL |
ROTOR INPUT ELECTRICAL POWER RATING | 7.8 WATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ZRO RESISTANCE IN OHMS | 9.10 NOMINAL |
PLUS J ZRO REACTANCE IN OHMS | 119.00 NOMINAL |
ZSO RESISTANCE IN OHMS | 8.20 NOMINAL |
PLUS J ZSO REACTANCE IN OHMS | 61.50 NOMINAL |
ZRS RESISTANCE IN OHMS | 12.00 NOMINAL |
PLUS J ZRS REACTANCE IN OHMS | 9.62 NOMINAL |
ZSO-90 RESISTANCE IN OHMS | 6.16 NOMINAL |
PLUS J ZSO-90 REACTANCE IN OHMS | 21.70 NOMINAL |
TRANSFORMATION RATIO | 0.783 ROTOR TO STATOR NOMINAL |
MAXIMUM TEMP RISE | 65.0 DEG CELSIUS |
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 75.00 OUTPUT |
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 100.00 |
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M8.0/P8.0 |
RECEIVER ERROR ANGULAR RANGE IN MINUTES | M60.0/P60.0 |
TORQUE GRADIENT PER ANGULAR DEG | 0.130 INCH-OUNCES NOMINAL |
BODY STYLE | STANDARD ROUND D |
SHOULDER DIAMETER | 1.9850 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM |
PILOT DIAMETER | 0.5900 INCHES MINIMUM AND 0.6000 INCHES MAXIMUM |
SECOND SHOULDER DIAMETER | 1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM |
SECOND SHOULDER LENGTH | 0.1680 INCHES MINIMUM AND 0.1700 INCHES MAXIMUM |
OVERALL LENGTH | 4.2940 INCHES MAXIMUM |
FLANGE DIAMETER | 2.2490 INCHES MINIMUM AND 2.2500 INCHES MAXIMUM |
FLANGE THICKNESS | 0.2480 INCHES MINIMUM AND 0.2500 INCHES MAXIMUM |
BODY DIAMETER | 1.9850 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM |
PILOT LENGTH | 0.0360 INCHES MINIMUM AND 0.0460 INCHES MAXIMUM |
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 | 3.4450 INCHES MAXIMUM |
ALIGNMENT HOLE DEPTH | 0.1250 INCHES NOMINAL |
ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 1.6420 INCHES NOMINAL |
ALIGNMENT HOLE QUANTITY | 3 |
TERMINAL TYPE AND QUANTITY | 5 SCREW |
TERMINAL LOCATION | REAR |
BODY MATERIAL | STEEL, STAINLESS |
SPECIAL FEATURES | SLOTTED KEYWAY FULL LENGTH OF SHAFT |
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 94 GOVERNMENT SPECIFICATION |