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SEMINAR ON ION DRIVE ENGINE
AMAN MISHRA
EEE
19C91A0202
Challenges
Objective
What Is Ion
How It Works
Application
The Future
Overview
___________________________________
The Challenges In The Field Of Space
Mission
Chemical thrusters such as fuels can’t give much power for long mission
it is unreliable , that it need frequent refueling
Solar energy is abundantly available in space , but can’t utilize it
completely
Fast moving shuttles are needed
A sustainable energy conversion system have to find out
Chemical
thruster
Solar
energy
Asteroids
what are the present objective?
Replacing
chemical
thruster
Self
charging
shuttle
study
about
other
nebula
Mission
to mars
High
power
engine
Can provide higher spacecraft top speeds than any rocket
currently available
Efficient use of fuel and electrical power enable modern space
craft to travel more
Why an ion engine ?
Cheaper and faster than any other propulsion technology
What is an ion ?
 Ion is simply an atom or molecule that is electrically charged
Ionization is the process of charging an atom
A gas is considered as ionized when some or all atoms are
converted to ion
plasma is known as the fourth state and in that state gas is neutral
It has the some properties of gas ,but affected with magnetic and
electrical properties
How does it work ?
 The mechanism uses charged particles to propel
aircraft forward.
 Operate relies on charge to mass ratio of
electrons.
 A cathode filament in a chamber with inert gases.
 The gases are charged by filament
Accelerated by the grid downstream
electrons are collected through a tube
the second grid accelerates the ion to 35km/s
In operation typically consume 1-7kw pf power ,have
exhaust velocities around 20-50 km/s
Layout 2
behaviour of plasma in magneticfield (slomo)
video 1
NASA LEWIS Research
Center
Why xenon is used?
 Xenon is an inert gas and thus corrosion can be avoided
First Ionization energy of xenon is 125eV/ato
No risk of explosions with high strorage density
Over the course of the 5.5+ year test,the engine consumed approximately
870 kilograms of xenon propellant.
hvdc
Simulated drone
producing
thrust to lift thin
aluminium foil
First ion drone flight
video 2
A picture is worth a thousand words

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aman.pptx

  • 1. SEMINAR ON ION DRIVE ENGINE AMAN MISHRA EEE 19C91A0202
  • 2. Challenges Objective What Is Ion How It Works Application The Future Overview ___________________________________
  • 3. The Challenges In The Field Of Space Mission Chemical thrusters such as fuels can’t give much power for long mission it is unreliable , that it need frequent refueling Solar energy is abundantly available in space , but can’t utilize it completely Fast moving shuttles are needed A sustainable energy conversion system have to find out Chemical thruster Solar energy Asteroids
  • 4. what are the present objective? Replacing chemical thruster Self charging shuttle study about other nebula Mission to mars High power engine
  • 5. Can provide higher spacecraft top speeds than any rocket currently available Efficient use of fuel and electrical power enable modern space craft to travel more Why an ion engine ? Cheaper and faster than any other propulsion technology
  • 6. What is an ion ?  Ion is simply an atom or molecule that is electrically charged Ionization is the process of charging an atom A gas is considered as ionized when some or all atoms are converted to ion plasma is known as the fourth state and in that state gas is neutral It has the some properties of gas ,but affected with magnetic and electrical properties
  • 7. How does it work ?  The mechanism uses charged particles to propel aircraft forward.  Operate relies on charge to mass ratio of electrons.  A cathode filament in a chamber with inert gases.  The gases are charged by filament
  • 8. Accelerated by the grid downstream electrons are collected through a tube the second grid accelerates the ion to 35km/s In operation typically consume 1-7kw pf power ,have exhaust velocities around 20-50 km/s
  • 9.
  • 11. behaviour of plasma in magneticfield (slomo) video 1
  • 13. Why xenon is used?  Xenon is an inert gas and thus corrosion can be avoided First Ionization energy of xenon is 125eV/ato No risk of explosions with high strorage density Over the course of the 5.5+ year test,the engine consumed approximately 870 kilograms of xenon propellant.
  • 14. hvdc
  • 15. Simulated drone producing thrust to lift thin aluminium foil First ion drone flight
  • 17. A picture is worth a thousand words