NSN 5990-00-330-5412
Part Details | ELECTRICAL RESOLVER
5990-00-330-5412 An item consisting of a rotor and a stator inductively coupled. It usually has two rotor windings displaced from each other by 90 degrees and two stator windings similarly displaced. The output voltage(s) is a trigonometric function of the input voltage(s) and the angular displacement of the rotor with respect to the stator. See also SYNCHRO (as modified) and GONIOMETER, ELECTRICAL. Excludes TRANSOLVER, ELECTRICAL and potentiometer sine/cosine electrical resolvers.
Alternate Parts: 10033253, VRB23414C, VRB23/41-4C, VRB234A, VRB23-4A, A3002668, MILR14346, 23R3N4, 23RS4A, MS510791, MS51079-1, 10033253, 113D2G, 7677411, 5990-00-330-5412, 00-330-5412, 5990003305412, 003305412
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1961 | 00-330-5412 | 22966 ( RESOLVER, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND D
Cross Reference | NSN 5990-00-330-5412
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 10033253 | 19204 | ARMY, UNITED STATES DEPARTMENT OFTHE |
| VRB23/41-4C | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| VRB23-4A | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| A3002668 | 28527 | HARRIS CORPORATIONDBA ELECTRONIC SYSTEMS, INTEGRATED |
| MILR14346 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 23R3N4 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 23RS4A | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MS51079-1 | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
| 10033253 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
| 113D2G | 97497 | UNITED AIRCRAFT CORPNORDEN DIVISION KETAY DEPT |
| 7677411 | 19200 | US ARMY ARDEC RDECOM |
Technical Data | NSN 5990-00-330-5412
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 23 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 90.0 MAXIMUM |
| STATOR INPUT CURRENT RATING | 445.0 MILLIAMPERES MAXIMUM |
| STATOR INPUT ELECTRICAL POWER RATING | 5.3 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZSO IMPEDANCE MAGNITUDE IN OHMS | 234.00 NOMINAL |
| ZSO IMPEDANCE ANGLE IN DEG | 83.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 16.50 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 4.70 NOMINAL |
| TRANSFORMATION RATIO | 1.027 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 1.300 INPUT TO OUTPUT NOMINAL |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 30.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 60.00 |
| BODY STYLE | STANDARD ROUND D |
| SHOULDER DIAMETER | 1.9850 INCHES MINIMUM AND 1.9950 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 | 0.1700 INCHES NOMINAL |
| OVERALL LENGTH | 4.7430 INCHES MINIMUM AND 4.7990 INCHES MAXIMUM |
| FLANGE DIAMETER | 2.2490 INCHES MINIMUM AND 2.2500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.2500 INCHES NOMINAL |
| BODY DIAMETER | 1.9850 INCHES MINIMUM AND 1.9950 INCHES MAXIMUM |
| PILOT LENGTH | 0.1090 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 | 4.0540 INCHES MINIMUM AND 4.0800 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 8 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| TEST DATA DOCUMENT | 81349-MIL-R-14346 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.). |
| FRAGILITY FACTOR | MODERATELY RUGGED |