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Ion thruster

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An ion thruster, also known as an ion drive or ion engine, is a type of electric propulsion used to move spacecraft. Unlike traditional chemical rockets that rely on combustion, these engines use electricity to accelerate charged particles to create thrust. This method is highly efficient because it uses a high exhaust velocity to move the vehicle. While the amount of force produced is very small, the efficiency is much higher than chemical alternatives.

Xenon ion engine prototype
Xenon ion engine prototype

This makes them ideal for long-duration missions in the vacuum of space.

The mechanism of an ion thruster relies on the principle of momentum conservation. First, a neutral gas, such as xenon, is introduced into a discharge chamber. The engine ionizes this gas by stripping electrons away from its atoms. This process can be done by bombarding the gas with energetic electrons from a hot cathode filament or by using an oscillating induced electric field. Once the gas becomes a collection of positive ions, they are accelerated out of the engine to create thrust.

Ion engine
Ion engine

To prevent the spacecraft from building up a negative charge, a neutralizer reinjects electrons into the ion beam. This ensures the exhaust remains electrically neutral so it can disperse freely.

Scientists categorize ion thrusters into two main types: electrostatic and electromagnetic. Electrostatic thrusters, such as gridded electrostatic ion engines, use the Coulomb force to accelerate ions. In these systems, the ionization process is physically separate from the acceleration process. Ions are pulled through a series of multi-aperture grids, moving from a screen grid to an accelerator grid. In contrast, electromagnetic thrusters use the Lorentz force to accelerate ions. These are often called plasma propulsion engines because the electric field is not in the direction of the acceleration.

Wfm hall thruster
Wfm hall thruster

The history of ion propulsion began with theoretical ideas long before working models existed. Konstantin Tsiolkovsky first suggested the concept in 1911 for use in near-vacuum conditions. In 1929, Hermann Oberth published thoughts on how electric propulsion could save mass in spacecraft. The idea gained popularity through science fiction, specifically a 1947 story by Jack Williamson. The first working ion thruster was built by Harold R. Kaufman in 1959 at the NASA Glenn Research Center. His model used mercury as a propellant and paved the way for future suborbital tests.

SERT-1 spacecraft
SERT-1 spacecraft

Testing these engines has led to several successful space missions. In 1964, the SERT-1 spacecraft successfully operated an ion engine for 31 minutes. Later, the Voskhod 1 spacecraft carried out tests with thrusters attached to its exterior. More recently, the Deep Space 1 mission in 1998 used an NSTAR thruster to change its velocity using xenon. The Dawn spacecraft also utilized ion propulsion in 2007 to achieve its mission goals.

These missions demonstrate how steady, low thrust can achieve significant results over time.

In terms of performance, ion thrusters operate with specific technical characteristics. They typically consume between 1 and 7 kilowatts of power. Their exhaust velocities are quite high, ranging from 20 to 50 kilometers per second. While their thrust is low, often between 25 and 250 millinewtons, their propulsive efficiency is high, between 65% and 80%. For comparison, the thrust from the Deep Space 1 engine was roughly equal to the weight of a single sheet of paper.

NEXIS thruster working
NEXIS thruster working

Although they cannot lift a craft off a planet, they provide sustained acceleration in space.

Because they produce such low thrust, ion engines are generally impractical for use within an atmosphere. The minuscule force cannot overcome air resistance without radical design changes. However, MIT researchers have worked on designs using ultra-light materials to fly at low speeds at ground level. In deep space, however, they are essential. They are used for satellite orientation, main propulsion for robotic vehicles, and even for crewed stations like the Tiangong. They represent a shift from the high-thrust, short-duration burns of chemical rockets to long-term, efficient travel.

Xenon ion engine prototype
Xenon ion engine prototype
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🖼️ Images & Media (7)
File:Ion Engine Test Firing - GPN-2000-000482.jpg
Ion Engine Test Firing - GPN-2000-000482.jpg
File:NEXIS thruster working.jpg
NEXIS thruster working.jpg
File:Xenon ion engine prototype.png
Xenon ion engine prototype.png
File:SERT-1 spacecraft.jpg
SERT-1 spacecraft.jpg
File:Ion engine.svg
Ion engine.svg
File:Wfm hall thruster.svg
Wfm hall thruster.svg
File:Average propulsive efficiency of rockets.png
Average propulsive efficiency of rockets.png
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