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$10 USD / hour
Flag of EGYPT
cairo, egypt
$10 USD / hour
It's currently 2:49 PM here
Joined November 29, 2017
0 Recommendations

Emad Eldeen A.

@Emadeldeen2017

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$10 USD / hour
Flag of EGYPT
cairo, egypt
$10 USD / hour
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Aerospace and Mechanical design engineer

Hello, Thank you for visiting my profile * I am an Aerospace and Mechanical engineer *Engineering >Aerospace >Mechanical >Electrical *Programming >Matlab >C++ >Mikro C >Arduino *Computational programs >Femap >Lumerical (FDTD-DEVICE) >Maple * Embedded systems >Homeautomation >Using different type of Sensors >Electric circuit design >PCB layout >Boards manufacture *Microcontroller >Pic microcontroller >AVR microcontroller >Arduino boards *Simulation programs >Proteus >Labview *CAD >SolidWorks >Autocad *Just look at my portfolio to check my proficiency and give me chance to demonstrate my ability to complete your project with a fair price within deadline. if you hire me you are awarded of the following 1-High quality and professional work 2-Well formatted Papers and presentations 3-Good customer service
Freelancer Translators Egypt
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Portfolio

4228235
Design a smart power distribution for a driver-less car
Design a smart power distribution for a driver-less car
4227715
Airplane design project by using matlab code
4227705
1-Magnetic torquer It is a satellite system for attitude control, built from electromagnetic coils. They generate a magnetic field when an electric current is applied. The magnetic field developed by the magnetorquers interacts with the earth's magnetic field to produce torque that we will use to rotate the satellite. 2-Reaction wheel The orientation requirements of a satellite (also referred to as spacecraft (are determined by its mission: telecommunications, optical imagery and meteorology to name a few. The mission also dictates the orientation of various satellite hardware components. 3-Power subsystem In this report we will make a successful fulfillment the design of electrical power subsystem for our universat-1. for any electrical power system there are some important requirements must be acquired and their requirements from the spacecraft requirements
Prototype for small satellite subsystems
1-Magnetic torquer It is a satellite system for attitude control, built from electromagnetic coils. They generate a magnetic field when an electric current is applied. The magnetic field developed by the magnetorquers interacts with the earth's magnetic field to produce torque that we will use to rotate the satellite. 2-Reaction wheel The orientation requirements of a satellite (also referred to as spacecraft (are determined by its mission: telecommunications, optical imagery and meteorology to name a few. The mission also dictates the orientation of various satellite hardware components. 3-Power subsystem In this report we will make a successful fulfillment the design of electrical power subsystem for our universat-1. for any electrical power system there are some important requirements must be acquired and their requirements from the spacecraft requirements
Prototype for small satellite subsystems
1-Magnetic torquer It is a satellite system for attitude control, built from electromagnetic coils. They generate a magnetic field when an electric current is applied. The magnetic field developed by the magnetorquers interacts with the earth's magnetic field to produce torque that we will use to rotate the satellite. 2-Reaction wheel The orientation requirements of a satellite (also referred to as spacecraft (are determined by its mission: telecommunications, optical imagery and meteorology to name a few. The mission also dictates the orientation of various satellite hardware components. 3-Power subsystem In this report we will make a successful fulfillment the design of electrical power subsystem for our universat-1. for any electrical power system there are some important requirements must be acquired and their requirements from the spacecraft requirements
Prototype for small satellite subsystems
1-Magnetic torquer It is a satellite system for attitude control, built from electromagnetic coils. They generate a magnetic field when an electric current is applied. The magnetic field developed by the magnetorquers interacts with the earth's magnetic field to produce torque that we will use to rotate the satellite. 2-Reaction wheel The orientation requirements of a satellite (also referred to as spacecraft (are determined by its mission: telecommunications, optical imagery and meteorology to name a few. The mission also dictates the orientation of various satellite hardware components. 3-Power subsystem In this report we will make a successful fulfillment the design of electrical power subsystem for our universat-1. for any electrical power system there are some important requirements must be acquired and their requirements from the spacecraft requirements
Prototype for small satellite subsystems
4226031
Concept Demonstration Prototype for small satellite
4228235
Design a smart power distribution for a driver-less car
Design a smart power distribution for a driver-less car
4227715
Airplane design project by using matlab code
4227705
1-Magnetic torquer It is a satellite system for attitude control, built from electromagnetic coils. They generate a magnetic field when an electric current is applied. The magnetic field developed by the magnetorquers interacts with the earth's magnetic field to produce torque that we will use to rotate the satellite. 2-Reaction wheel The orientation requirements of a satellite (also referred to as spacecraft (are determined by its mission: telecommunications, optical imagery and meteorology to name a few. The mission also dictates the orientation of various satellite hardware components. 3-Power subsystem In this report we will make a successful fulfillment the design of electrical power subsystem for our universat-1. for any electrical power system there are some important requirements must be acquired and their requirements from the spacecraft requirements
Prototype for small satellite subsystems
1-Magnetic torquer It is a satellite system for attitude control, built from electromagnetic coils. They generate a magnetic field when an electric current is applied. The magnetic field developed by the magnetorquers interacts with the earth's magnetic field to produce torque that we will use to rotate the satellite. 2-Reaction wheel The orientation requirements of a satellite (also referred to as spacecraft (are determined by its mission: telecommunications, optical imagery and meteorology to name a few. The mission also dictates the orientation of various satellite hardware components. 3-Power subsystem In this report we will make a successful fulfillment the design of electrical power subsystem for our universat-1. for any electrical power system there are some important requirements must be acquired and their requirements from the spacecraft requirements
Prototype for small satellite subsystems
1-Magnetic torquer It is a satellite system for attitude control, built from electromagnetic coils. They generate a magnetic field when an electric current is applied. The magnetic field developed by the magnetorquers interacts with the earth's magnetic field to produce torque that we will use to rotate the satellite. 2-Reaction wheel The orientation requirements of a satellite (also referred to as spacecraft (are determined by its mission: telecommunications, optical imagery and meteorology to name a few. The mission also dictates the orientation of various satellite hardware components. 3-Power subsystem In this report we will make a successful fulfillment the design of electrical power subsystem for our universat-1. for any electrical power system there are some important requirements must be acquired and their requirements from the spacecraft requirements
Prototype for small satellite subsystems
1-Magnetic torquer It is a satellite system for attitude control, built from electromagnetic coils. They generate a magnetic field when an electric current is applied. The magnetic field developed by the magnetorquers interacts with the earth's magnetic field to produce torque that we will use to rotate the satellite. 2-Reaction wheel The orientation requirements of a satellite (also referred to as spacecraft (are determined by its mission: telecommunications, optical imagery and meteorology to name a few. The mission also dictates the orientation of various satellite hardware components. 3-Power subsystem In this report we will make a successful fulfillment the design of electrical power subsystem for our universat-1. for any electrical power system there are some important requirements must be acquired and their requirements from the spacecraft requirements
Prototype for small satellite subsystems
4226031
Concept Demonstration Prototype for small satellite

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Experience

Airplane design/maintenance

Egyptian air force
Feb 2017 - Present
I am an Aerospace and Mechanical design engineer .having 3 years of experience in Airplane design/maintenance in Egyptian Air force

Education

graduated

Cairo University, Egypt 2011 - 2016
(5 years)

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Top Skills

Translation
Video Services
Excel
Matlab and Mathematica
Microcontroller

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