NSN 5990-00-099-0700
Part Details | ELECTRICAL RESOLVER
5990-00-099-0700 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: 9V11R41N40A, 9V-11R41N40A, MILR2341725, MIL-R-23417/25, 5990-00-099-0700, 00-099-0700, 5990000990700, 000990700
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | DEC 13, 1972 | 00-099-0700 | 22966 ( RESOLVER, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-099-0700
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9V-11R41N40A | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-R-23417/25 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 5990-00-099-0700
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 9.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 2.6 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 10.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 4000.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 3720.00 MINIMUM AND 4467.00 MAXIMUM |
| ZSS RESISTANCE IN OHMS | 121.00 MINIMUM AND 145.00 MAXIMUM |
| ZRO IMPEDANCE MAGNITUDE IN OHMS | 68.00 MINIMUM AND 73.00 MAXIMUM |
| ZSS IMPEDANCE MAGNITUDE IN OHMS | 65.00 MINIMUM AND 69.00 MAXIMUM |
| TRANSFORMATION RATIO | 0.497 ROTOR TO STATOR NOMINAL |
| MAXIMUM TEMP RISE | 85.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 15.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 20.00 |
| INTERAXIS ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 2.4130 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.0570 INCHES MINIMUM AND 1.0650 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.9745 INCHES MINIMUM AND 0.9750 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
| PILOT LENGTH | 0.0620 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 2.3340 INCHES MINIMUM AND 2.3540 INCHES MAXIMUM |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8090 INCHES MINIMUM AND 0.8150 INCHES MAXIMUM |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 7 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| TEST DATA DOCUMENT | 81349-MIL-R-23417 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-R-23417 TO 25 GOVERNMENT SPECIFICATION |