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How Would New Plasma-Powered Spaceships Work?

A higher thrust

By Lucian Dorneanu, Science Editor & Stefan Anitei, Science Editor

14th of June 2007, 15:24 GMT

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Future plasma-powered spaceship
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A new plasma rocket design underwent thorough testing and eventually broke the endurance record for its class, and could provide the next generation of propulsion systems for future space missions.

Plasma propulsion engines use accelerated plasma
for propulsion. Though far less powerful than conventional atmospheric rocket engines, plasma engines are able to operate at higher efficiencies and for longer periods of time, and are better suited for long-distance inter-planetary space travel missions

The manufacturers of the rocket, Ad Astra Rocket Company, said they hope this type of rocket will soon become cheaper to operate than conventional models and will reduce travel time for space missions.

It works by tearing electrons from hydrogen atoms to produce the ionized gas, and then by propelling them in an electric field, which accelerates the plasma and expels it out of the back of the engine at high speeds, a process which is reflected in the overall high speed of the craft equipped with this type of engine.

One technique, called variable specific impulse magnetoplasma rocket (VASIMR) is a form of spacecraft propulsion that uses radio waves and magnetic fields to accelerate a propellant, and current designs can produce specific impulses ranging from 10 to 300, but only four hours of continuous flight.

Currently, there are hundreds of plasma thrusters in use, most of them used on satellites for stationkeeping. Plasma thrusters have also been used for deep space missions, including Deep Space 1, which demonstrated continuous firing of a xenon gridded ion thruster for 25,000 hours (almost three years straight), but VASMIR is unique because it has a much lower Isp and a much higher thrust than conventional plasma/electric propulsion devices, which increases the operational envelope of electric propulsion devices.

One of the advantages of this rocket is the fact that it can accelerate continuously, unlike conventional rockets, that generate all their thrust in the first few minutes of a mission and then coast to their destination.

There are significant challenges ahead, the space ships of the future, equipped with these engines, would experience greatly reduced travel times and could also provide a low level of artificial gravity for astronauts, while using hydrogen as fuel, common throughout the universe, and available for harvesting en route.

TAGS:

plasma | engine | ship | rocket
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User opinions:


Comment #1 by: MM on 17 Dec 2007, 22:00 GMT reply to this comment

There are quite a few things in this article that need clarification. The most obvious: specific impulse, Isp, is measured in seconds (exit velocity (m/s) divided by acceleration of gravity on earth (m/s^2)) It is unclear from this article whether the Isp quoted is actually exit velocity or the units were misquoted. I would guess the units were misquoted just from the magnitudes reported.

A little more subtle point: this thruster (VASMIR) is not the only type of plasma thruster. There are hundreds of plasma thrusters in use, mostly on satellites for stationkeeping. Plasma thrusters have also been used for deep space missions, including Deep Space 1, which demonstrated continuous firing of a xenon gridded ion thruster for 25,000 hours (almost three years straight). That makes the four hour burn seem pretty small.

The way VASMIR is unique is that it has a much lower Isp and a much higher thrust than conventional plasma/electric propulsion devices, which extends the operational envelope of electric propulsion devices. This article misses this point entirely.


Comment #2 by: Ken on 10 Jan 2009, 22:59 GMT reply to this comment

They are talking about Propelling a ship in space. The Laws of gravity does not aply here.


Comment #3 by: Tinsae on 23 Jul 2009, 14:42 GMT reply to this comment

if the propeller medium is ionized and the whole craft ejecting charges. will the separated charges (the ejected and the craft left charge) decellerate the craft because of mutual attraction?

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