Does this plasma-powered 100,000 MPH rocket engine reduces the Mars travel time to half?

Category: SCIENCE

Asked on 2020-02-21 07:16:51
Viewed 173 times
Asked by Pendulum World


The answer

Pendulum World wrote on 21st of February 2020
Yes, it does !

 

Pendulum World wrote on 21st of February 2020
This will be the rocket engine of the future !

 


Useful links on topic - More information - Source

https://www.express.co.uk/news/science/1240294/science-news-mars-space-travel-nuclear-fusion-plasma-brexit-space-sector-made-in-chelsea?fbclid=IwAR25KT1TDLAJeXSMBBeqzh3rluYDWjh1HTb9w1_2iE3MY0UhKEADcTniJwU
https://en.wikipedia.org/wiki/Plasma_propulsion_engine

The story

A plasma propulsion engine is a type of electric propulsion that generates thrust from a quasi-neutral plasma. This is in contrast to ion thruster engines, which generate thrust through extracting an ion current from the plasma source, which is then accelerated to high velocities using grids/anodes. These exist in many forms (see electric propulsion). Plasma thrusters do not typically use high voltage grids or anodes/cathodes to accelerate the charged particles in the plasma, but rather uses currents and potentials which are generated internally in the plasma to accelerate the plasma ions. While this results in a lower exhaust velocity by virtue of the lack of high accelerating voltages, this type of thruster has a number of advantages. The lack of high voltage grids of anodes removes a possible limiting element as a result of grid ion erosion. The plasma exhaust is 'quasi-neutral', which means that ions and electrons exist in equal number, which allows simple ion-electron recombination in the exhaust to neutralize the exhaust plume, removing the need for an electron gun (hollow cathode). This type of thruster often generates the source plasma using radio frequency or microwave energy, using an external antenna. This fact, combined with the absence of hollow cathodes (which are very sensitive to all but the few noble gases) allows the intriguing possibility of being able to use this type of thruster on a huge range of propellants, from argon, to carbon dioxide, air mixtures, to astronaut urine.

 

source text and image : https://en.wikipedia.org

(*) Lines marked in red are not the truth.

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