NSN 5990-00-929-0500
Part Details | TRANSMITTER SYNCHRO
5990-00-929-0500 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the stator into a receiver synchro, a control transformer or differential synchro is dependent upon the position of its rotor. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: 18CX1253, 1136443, 18CX4D, VCX184N1, VCX18-4N1, 18CX46, M2070828D001, M20708/28D-001, M207082801D, M20708/28-01D, M2070821D001, M20708-21D001, MILS2070828, MIL-S-20708/28, 18CX4D, 18CX4B, 45090029942, 450900-2994-2, 4509002994002, 450900-2994-002, 2.012948, 1,792351, 59 000014, 59 000-014, M207082801D, M20708/28-01D, AS2070828, AS20708/28, N14503, 352250005254, VBE41510, VBE415-10, 5990-00-929-0500, 00-929-0500, 5990009290500, 009290500
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | SEP 02, 1966 | 00-929-0500 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-929-0500
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 18CX1253 | 14404 | AMETEK TECHNICAL & INDUSTRIALPRODUCTS, INC. |
| 1136443 | 82205 | BELFORT INSTRUMENT COMPANY |
| 18CX4D | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| VCX18-4N1 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| 18CX46 | 54497 | MARTIN MARIETTA TECHNOLOGIES INCSUB OF MARTIN MARIETTA CORP |
| M20708/28D-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/28-01D | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708-21D001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-20708/28 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 18CX4D | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 18CX4B | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 450900-2994-2 | D4856 | NORTHROP GRUMMAN LITEF GMBHDBA LITEF |
| 450900-2994-002 | D4856 | NORTHROP GRUMMAN LITEF GMBHDBA LITEF |
| 2.012948 | D2865 | RAYTHEON ANSCHUETZ GMBHDBA RAYTHEON ELECTRICS GMBH |
| 1,792351 | D2865 | RAYTHEON ANSCHUETZ GMBHDBA RAYTHEON ELECTRICS GMBH |
| 59 000-014 | D9853 | ROCKWELL COLLINS DEUTSCHLANDSERVICES GMBH |
| M20708/28-01D | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AS20708/28 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| N14503 | 81574 | TCE CANADA LTD |
| 352250005254 | H0203 | THALES NEDERLANDDBA THALES LAND & JOINT SYSTEMS |
| VBE415-10 | H0203 | THALES NEDERLANDDBA THALES LAND & JOINT SYSTEMS |
Technical Data | NSN 5990-00-929-0500
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 18 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 110.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 900.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO IMPEDANCE MAGNITUDE IN OHMS | 1045.00 MINIMUM AND 1400.00 MAXIMUM |
| ZRO IMPEDANCE ANGLE IN DEG | 84.00 MINIMUM AND 87.50 MAXIMUM |
| ZSS IMPEDANCE MAGNITUDE IN OHMS | 40.00 MINIMUM AND 57.00 MAXIMUM |
| ZSS IMPEDANCE ANGLE IN DEG | 34.00 MINIMUM AND 48.00 MAXIMUM |
| TRANSFORMATION RATIO | 0.785 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 1.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 20.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 40.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 60.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M6.0/P6.0 |
| TORQUE GRADIENT PER ANGULAR DEG | 0.100 INCH-OUNCES MAXIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 1.5615 INCHES MINIMUM AND 1.5620 INCHES MAXIMUM |
| PILOT DIAMETER | 0.0375 INCHES NOMINAL |
| OVERALL LENGTH | 3.0600 INCHES NOMINAL |
| FLANGE DIAMETER | 1.7450 INCHES MINIMUM AND 1.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 1.6250 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0780 INCHES NOMINAL |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| SHOULDER LENGTH | 0.1320 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 2.5200 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES MINIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 1.2500 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL |
| 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 28 GOVERNMENT SPECIFICATION |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| FRAGILITY FACTOR | MODERATELY RUGGED |
| END ITEM IDENTIFICATION | GUN FIRE CONTROL SYSTEM, MK 68; TICONDEROGA CLASS CG (47); FORRESTAL CLASS CV; LOS ANGELES CLASS SSN (688); NIMITZ CLASS CVN; KIDD CLASS DDG; STURGEON CLASS SSN (637); VIRGINIA CLASS CGN (41); SPRUANCE CLASS DD (963) |
