5M451-1A10
Transmitter Synchro
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.
standard round a body style, 0.0620 inches nominal flange thickness, 1.7250 inches maximum overall length, 0.7450 inches minimum and 0.7530 inches maximum flange diameter, 0.4995 inches minimum and 0.5000 inches maximum pilot diameter
Basic Details
View the essential basic details of this aerospace electrical component, including key identifiers and classifications.
5990-00-578-7452
00-578-7452
Transmitter Synchro
5M451-1A10
5990 - Synchros and Resolvers
Electrical and Electronic Equipment Components
01/01/1963 (63 years ago)
02073
Technical Specifications
Review the complete technical specifications, performance details, and compliance standards for aerospace electrical component: 5M451-1A10
- Body Style
- standard round a
- Pilot Diameter
- 0.4995 inches minimum and 0.5000 inches maximum
- Overall Length
- 1.7250 inches maximum
- Flange Diameter
- 0.7450 inches minimum and 0.7530 inches maximum
- Flange Thickness
- 0.0620 inches nominal
- Undercut Diameter
- 0.6870 inches nominal
- Undercut Width
- 0.0620 inches nominal
- Shaft Diameter
- 0.1195 inches minimum and 0.1200 inches maximum single shaft
- Shaft Length
- 0.4610 inches minimum and 0.4850 inches maximum single shaft
- Body Size
- 8
- Rotor Input Voltage Rating In Volts
- 26.0 nominal
- Frequency In Hertz
- 400.0 nominal
- Rotor Input Current Rating
- 114.0 milliamperes nominal
- Rotor Input Electrical Power Rating
- 800.0 milliwatts nominal
- Zro Resistance In Ohms
- 70.00 nominal
- Zso Resistance In Ohms
- 17.00 nominal
- Rotor Dc Resistance In Ohms
- 59.00 nominal
- Stator Dc Resistance In Ohms
- 18.00 nominal
- Phase Shift Angle In Deg
- 13.000 input to output nominal
- Maximum Fundamental Null Voltage In Millivolts Per Volt
- 15.00 output
- Maximum Total Null Voltage Output In Millivolts Per Volt
- 20.00
- Electrical Error Angular Range In Minutes
- -7.0 to 7.0
- Pilot Length
- 0.0400 inches nominal
- Mounting Surface To Terminal End Distance
- 1.2400 inches maximum
- Body Material
- steel corrosion resisting
- Terminal Location
- rear
- Plus J Zro Reactance In Ohms
- 260.00 nominal
- Shaft Slot Depth
- 0.0300 inches nominal single shaft
- Plus J Zso Reactance In Ohms
- 49.00 nominal
- Shaft Slot Width
- 0.0250 inches nominal single shaft
- Shaft Type
- round, slotted single shaft
- Transformation Ratio
- 0.454 rotor to stator nominal
- Terminal Type And Quantity
- 5 wire lead
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Cross Referenced Parts
Our Cross-Referenced Parts section helps you quickly locate compatible or equivalent aerospace electrical components for: 5M451-1A10
| Part Number | CAGE | Manufacturer | RNCC | RNVC | RNAAC |
|---|---|---|---|---|---|
| 5M451-1A10 | 76301 | The Boeing Company Div Defense | 5 | 2 | XX |
| 825191 | 10001 | Navair and Navsea Managed Original Design Activity Dwg Not Material/parts Supplier | C | 1 | ZZ |
| 910083-7 | 06481 | Northrop Grumman Systems Corporation Div the Navigation, Targeting and Survivability Division | C | 1 | ZZ |
| G355635-1 | 23667 | Smiths Detection Inc. Dba Smiths Detection Inc Casc Div Edgewood | C | 1 | ZZ |
| PS960100002-1 | 38597 | Lockheed Martin Corporation Div Rotary and Mission Systems | 5 | 2 | XX |
| R1011-1A | 88818 | Kearfott Corporation Div Guidance and Navigation Division | 3 | 2 | XX |
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