Part Details | TRANSMITTER SYNCHRO
5990-00-070-8522 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: 760091500, 76-00915-00, 23CX4A, VCX234N3, VCX23-4N3, WD6368ITEM15, S0C4010, 397001023, 397-001-023, 23CX4D, 73783414, 737834-14, S0C4010, WD6368ITEM15, VTSN2364N223CX4D, VTSN23-64-N2/23CX4D, M28787219, M28787/219, M2070845D001, M20708/45D-001, M20708451D, M20708/45-1D, M207084501D, M20708/45-01D, M207084501, M20708/45-01, M2070845001, M20708/45-001, MILS2070845, MIL-S-20708/45, 23CX4D, 23M1H1Q, 8212801, 5612397, D10760, AS2070845, AS20708/45, VTSN2364N223CX4D, VTSN23-64-N2/23CX4D, 99053917, 069732130, 5990-00-070-8522, 00-070-8522, 5990000708522, 000708522
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JUL 20, 1967 | 00-070-8522 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND D
Cross Reference | NSN 5990-00-070-8522
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 76-00915-00 | S3012 | CONSILIUM MARINE & SAFETY AB,NAVIGATION |
| 23CX4A | S3012 | CONSILIUM MARINE & SAFETY AB,NAVIGATION |
| VCX23-4N3 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| WD6368ITEM15 | 89914 | I-T-E IMPERIAL CORP SUBSIDIARY OFGOULD INC ATLANTA MARINE DEPT |
| S0C4010 | 89914 | I-T-E IMPERIAL CORP SUBSIDIARY OFGOULD INC ATLANTA MARINE DEPT |
| 397-001-023 | 07421 | INTERSTATE ELECTRONICS CORPORATIONDBA L-3 INTERSTATE ELECTRONICS |
| 23CX4D | 80058 | JOINT ELECTRONICS TYPE DESIGNATIONSYSTEM |
| 737834-14 | 11447 | L3 TECHNOLOGIES, INC.DBA COMMUNICATION SYSTEMS - EAST |
| S0C4010 | 28199 | L3 TECHNOLOGIES, INC.DBA L3 HENSCHEL |
| WD6368ITEM15 | 28199 | L3 TECHNOLOGIES, INC.DBA L3 HENSCHEL |
| VTSN23-64-N2/23CX4D | 28199 | L3 TECHNOLOGIES, INC.DBA L3 HENSCHEL |
| M28787/219 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/45D-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/45-1D | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/45-01D | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/45-01 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/45-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-20708/45 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 23CX4D | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 23M1H1Q | K0624 | MUIRHEAD AEROSPACE LTDDBA MUIRHEAD AVIONICS |
| 8212801 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 5612397 | 53711 | NAVAL SEA SYSTEMS COMMAND |
| D10760 | 95542 | NORTHROP GRUMMAN SYSTEMS CORPORATION |
| AS20708/45 | 0VH01 | SAE CUSTOMER SERVICEDEPT 2045 |
| VTSN23-64-N2/23CX4D | 96264 | TEN BOSCH M INC |
| 99053917 | F6481 | THALES SA |
| 069732130 | D1876 | WAERTSILAE ELAC NAUTIK GMBH |
Technical Data | NSN 5990-00-070-8522
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 23 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 245.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 1.7 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO IMPEDANCE MAGNITUDE IN OHMS | 470.00 MINIMUM AND 580.00 MAXIMUM |
| ZRO IMPEDANCE ANGLE IN DEG | 84.00 MINIMUM AND 87.50 MAXIMUM |
| ZSS IMPEDANCE MAGNITUDE IN OHMS | 21.60 MINIMUM AND 26.00 MAXIMUM |
| ZSS IMPEDANCE ANGLE IN DEG | 42.00 MINIMUM AND 47.00 MAXIMUM |
| TRANSFORMATION RATIO | 0.783 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 1.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 20.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 32.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 48.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M6.0/P6.0 |
| TORQUE GRADIENT PER ANGULAR DEG | 0.200 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 | 4.2990 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| 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 45 GOVERNMENT SPECIFICATION |
| FRAGILITY FACTOR | MODERATELY RUGGED |