A3002668
Electrical Resolver
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.
1.9850 inches minimum and 1.9950 inches maximum shoulder diameter, 0.5900 inches minimum and 0.6000 inches maximum pilot diameter, steel, corrosion resisting body material, 1.9985 inches minimum and 1.9995 inches maximum second shoulder diameter, standard round d body style
Basic Details
View the essential basic details of this aerospace electrical component, including key identifiers and classifications.
5990-00-330-5412
00-330-5412
Electrical Resolver
A3002668
5990 - Synchros and Resolvers
Electrical and Electronic Equipment Components
01/01/1961 (65 years ago)
22966
Technical Specifications
Review the complete technical specifications, performance details, and compliance standards for aerospace electrical component: A3002668
- Body Material
- steel, corrosion resisting
- 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
- Shaft Diameter
- 0.2402 inches minimum and 0.2405 inches maximum single shaft
- Shaft Length
- 0.6930 inches minimum and 0.7190 inches maximum single shaft
- Fragility Factor
- moderately rugged
- 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
- 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
- Pilot Length
- 0.1090 inches nominal
- Shoulder Length
- unable to decode
- 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
- Shaft Thread Series Designator
- unf single shaft
- Shaft Thread Direction
- right-hand single shaft
- Shaft Thread Class
- 2a single shaft
- Terminal Location
- rear
- Shaft Thread Length
- 0.3100 inches minimum and 0.3400 inches maximum single shaft
- Shaft Type
- round, threaded single shaft
- Transformation Ratio
- 1.027 rotor to stator nominal
- Shaft Nominal Thread Size
- 0.240 inches single shaft
- 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.)."
- Terminal Type And Quantity
- 8 screw
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Cross Referenced Parts
Our Cross-Referenced Parts section helps you quickly locate compatible or equivalent aerospace electrical components for: A3002668
| Part Number | CAGE | Manufacturer | RNCC | RNVC | RNAAC |
|---|---|---|---|---|---|
| 10033253 | 18876 | Us Army Aviation and Missile Command | 5 | 1 | XX |
| 10033253 | 19204 | Army, United States Department of the Dba Rock Island Arsenal Jmtc | 5 | 1 | BF |
| 113D2G | 97497 | United Aircraft Corp Norden Division Ketay Dept | C | 1 | TX |
| 23R3N4 | 81349 | Military Specifications Promulgated by Military Departments/agencies Under Authority of Defense Standardization Manual 4120 3-M | 2 | 2 | TX |
| 23RS4A | 81349 | Military Specifications Promulgated by Military Departments/agencies Under Authority of Defense Standardization Manual 4120 3-M | C | 1 | ZZ |
| 23RS4A | 95542 | Northrop Grumman Systems Corporation | 3 | 2 | XX |
| 7677411 | 19200 | Combat Capabilities Development Command (ccdc) Armaments Center Dba Ccdc Div Logistics Research and Engineering Directorate | 5 | 1 | HH |
| A3002668 | 28527 | L3harris Technologies, Inc. | C | 1 | ZZ |
| MIL-R-14346 | 81349 | Military Specifications Promulgated by Military Departments/agencies Under Authority of Defense Standardization Manual 4120 3-M | 4 | 1 | ZZ |
| MIL-R-14346 | 81349 | Military Specifications Promulgated by Military Departments/agencies Under Authority of Defense Standardization Manual 4120 3-M | 4 | 1 | TX |
| MS51079-1 | 96906 | Military Standards Promulgated by Military Departments Under Authority of Defense Standardization Manual 4120 3-M | 5 | 9 | TX |
| VRB23-4A | 10112 | General Dynamics Motion Control Llc | C | 1 | TX |
| VRB23/41-4C | 10112 | General Dynamics Motion Control Llc | C | 1 | TX |
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