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Plasma propulsion engine

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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 positive ions and electrons exist in equal number, which allows simple ion-electron
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have attained ~2000 s. This is a significant improvement over the bipropellant fuels of conventional chemical rockets, which feature specific impulses ~450 s. With high impulse, plasma thrusters are capable of reaching relatively high speeds over extended periods of acceleration. Ex-astronaut
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Possibly the most significant challenge to the viability of plasma thrusters is the energy requirement. The VX-200 engine, for example, requires 200 kW electrical power to produce 5 N of thrust, or 40 kW/N. This power requirement may be met by fission reactors, but the reactor mass
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Due to their extremely low thrust, plasma engines are not suitable for launch-to-Earth-orbit. On average, these rockets provide about 2 pounds of thrust maximum. Plasma thrusters are highly efficient in open space, but do nothing to offset the orbit expense of chemical rockets.
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that wraps around a gas chamber creates waves and excites the gas, creating plasma. The plasma is expelled at high velocity to produce thrust via acceleration strategies that require various combinations of electric and magnetic fields of ideal
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to accelerate the charged particles in the plasma, but rather use currents and potentials that are generated internally to accelerate the ions, resulting in a lower exhaust velocity given the lack of high accelerating voltages.
312:. They belong to the category of electrodeless thrusters. These thrusters support multiple propellants, making them useful for longer missions. They can be made out of simple materials including a glass soda bottle. 181:
which carried six PPTs that served as actuators of the attitude control system. The PPT propulsion system was tested for 70 minutes on the 14 December 1964 when the spacecraft was 4.2 million kilometers from Earth.
370:(PIT) also use the Lorentz force to generate thrust, but they do not use electrodes, solving the erosion problem. Ionization and electric currents in the plasma are induced by a rapidly varying magnetic field. 197:. The thrust estimates published in that work, however, were subsequently shown to be almost nine times theoretically possible levels even if 100% of the input microwave power were converted to thrust. 265:
Certain plasma thrusters, such as the mini-helicon, are hailed for their simplicity and efficiency. Their theory of operation is relatively simple and can use a variety of gases, or combinations.
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Another challenge is plasma erosion. While in operation the plasma can thermally ablate the walls of the thruster cavity and support structure, which can eventually lead to system failure.
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satellite. The thruster was the satellite's main propulsion system. The company launched another hall effect thruster that year. In 2020, research on a plasma jet was published by
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Helicon plasma thrusters use low-frequency electromagnetic waves (Helicon waves) that exist inside plasma when exposed to a static magnetic field. An
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is producing the 200 kW RF generators required to ionize the propellant. Some component tests and "Plasma Shoot" experiments are performed in a
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thruster could send a payload to Mars in as little as 39 days while reaching a maximum velocity of 34 miles per second (55 km/s).
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The Costa Rican Aerospace Alliance announced the development of exterior support for the VASIMR to be fitted outside the
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Some plasma engines have seen active flight time and use on missions. The first use of plasma engines was a
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Dynamics and control of the vortex flow behind a slender conical forebody by a pair of plasma actuators
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plasma electrons and ions in the same direction, thereby operating without a neutralizer.
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recombination in the exhaust to neutralize the exhaust plume, removing the need for an
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Wright, Peter; Samples, Stephen; Uchizono, Nolan; Wirz, Richard (15 September 2020).
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These qualities suggest that plasma thrusters have value for many mission profiles.
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engines, which generate thrust through extracting an ion current from the
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VASIMR, short for Variable Specific Impulse Magnetoplasma Rocket, uses
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Many space agencies developed plasma propulsion systems, including the
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thruster can be throttled for an impulse greater than 12000 s, and
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Plasma thrusters do not typically use high voltage grids or anodes/
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source, which is then accelerated to high velocities using grids/
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Flow Separation Control over an Airfoil Using Plasma Co-Flow Jet
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laboratory. This project is led by former NASA astronaut Dr.
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then accelerates the plasma out of the engine, generating
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value than most other types of rocket technology. The
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to launch the first hall effect thruster aboard the
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(December 2018). 512:Plasma Sources Science and Technology 395:when under the influence of a strong 7: 474:Wingless Electromagnetic Air Vehicle 1954:Future-oriented technology analysis 598:"Plasma engine passes initial test" 136:Plasma engines are well-suited for 2047:Plasma technology and applications 1282:Field-emission electric propulsion 503:Mazouffre, Stéphane (2016-06-01). 234:Plasma engines have a much higher 25: 1356:Microwave electrothermal thruster 81:. These exist in many forms (see 2008: 1628: 1486:Pulsed nuclear thermal rocket‎ 1382:High Power Electric Propulsion 385:Electrodeless plasma thrusters 374:Electrodeless plasma thrusters 327:Magnetoplasmadynamic thrusters 316:Magnetoplasmadynamic thrusters 153:Australian National University 1: 1981:Technology in science fiction 1341:Helicon double-layer thruster 1310:Electrodeless plasma thruster 1305:Magnetoplasmadynamic thruster 532:10.1088/0963-0252/25/3/033002 380:Electrodeless plasma thruster 322:Magnetoplasmadynamic thruster 299:Helicon double-layer thruster 185:In 2011, NASA partnered with 41:A thruster during test firing 1826:Laser communication in space 928:Mini-Helicon Plasma Thruster 391:which acts on any plasma or 224:International Space Station 69:. This is in contrast with 34:Type of electric propulsion 2068: 1986:Technology readiness level 1922:Technological unemployment 922:Plasma Propulsion in Space 422: 377: 368:Pulsed inductive thrusters 360: 357:Pulsed inductive thrusters 319: 296: 203:is developing the VASIMR. 129:air mixtures to astronaut 113:energy, using an external 26: 2004: 1969:Technological singularity 1929:Technological convergence 1626: 1300:Pulsed inductive thruster 363:Pulsed inductive thruster 1831:Orbital propellant depot 1788:Plasma propulsion engine 1783:Nuclear pulse propulsion 1474:Nuclear pulse propulsion 1233:Electric-pump-fed engine 1133:Hybrid-propellant rocket 1123:Liquid-propellant rocket 705:South China Morning Post 648:Physics of Atomic Nuclei 293:Helicon plasma thrusters 59:plasma propulsion engine 1934:Technological evolution 1907:Exploratory engineering 1768:Beam-powered propulsion 1750:Reusable launch vehicle 1530:Beam-powered propulsion 1503:Fission-fragment rocket 1458:Nuclear photonic rocket 1426:Nuclear electric rocket 1192:Staged combustion cycle 1128:Solid-propellant rocket 578:. cbcnews. 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The 260:VASIMR 247:VASIMR 209:Nautel 176:Zond 2 173:Soviet 79:anodes 75:plasma 67:plasma 51:VASIMR 1814:Other 1370:Other 1116:State 750:S2CID 536:S2CID 508:(PDF) 187:Busek 131:urine 123:argon 2015:List 1100:WINE 660:2024 584:2012 562:2012 151:and 740:doi 528:doi 433:to 403:to 125:to 109:or 89:". 2033:: 877:. 853:. 829:. 818:^ 802:. 773:. 762:^ 748:. 738:. 728:10 726:. 722:. 703:. 679:. 668:^ 652:81 650:. 646:. 621:. 610:^ 600:. 534:. 526:. 516:25 514:. 510:. 437:a 353:. 241:sp 159:. 147:, 133:. 57:A 1668:e 1661:t 1654:v 966:e 959:t 952:v 907:. 887:. 863:. 839:. 812:. 788:. 756:. 742:: 734:: 689:. 662:. 631:. 586:. 564:. 542:. 530:: 522:: 243:) 238:I 31:. 20:)

Index

Plasma thruster
Plasma (engine)


VASIMR
electric propulsion
plasma
ion thruster
plasma
anodes
electric propulsion
ion engines
cathodes
electron gun
radio frequency
microwave
antenna
noble gases
argon
carbon dioxide
urine
interplanetary
European Space Agency
Iranian Space Agency
Australian National University
double layer thruster
Pulsed plasma thruster
Soviet
Zond 2
space probe

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