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A plasma magnet is a proposed spacecraft propulsion device that uses a dipole magnetic field to capture energy from the solar wind. The field acts as
Plasma_magnet
Proposed spacecraft propulsion method
the static magnetic dipole for a magnetic sail in a design called the Plasma magnet (PM) that was described as an AC induction motor turned inside out.
Magnetic_sail
Type of electric propulsion
A plasma propulsion engine is a type of electric propulsion that generates thrust from a quasi-neutral plasma. This is in contrast with ion thruster engines
Plasma_propulsion_engine
The electrodeless plasma thruster is a spacecraft propulsion engine commercialized under the acronym "E-IMPAcT" for "Electrodeless-Ionization Magnetized
Electrodeless_plasma_thruster
Magnetic confinement device used to produce thermonuclear fusion power
machine which uses a powerful magnetic field generated by external magnets to confine plasma in the shape of an axially symmetrical torus. The tokamak is the
Tokamak
Rocket driven by nuclear fusion power
fusing plasma) approaches. Like the magnetic approach, the fusion fuel is confined at low density by magnetic fields while it is heated into a plasma, but
Fusion_rocket
Type of propulsion for spacecraft
A pulsed plasma thruster (PPT) or as a plasma jet engine (PJE), is a form of electric spacecraft propulsion. PPTs are generally considered the simplest
Pulsed_plasma_thruster
Type of electric propulsion system
(Russian: СПД, стационарный плазменный двигатель; English: SPT, Stationary Plasma Thruster) at Design Bureau Fakel thrusters with narrow acceleration zone
Hall-effect_thruster
Physical and science fiction concept
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Anti-gravity
Proposed spacelaunch method
on December 1, 2012. Retrieved May 3, 2011. "Constant Acceleration". "Magnets, Not Rockets, Could Fling Satellites Into Space". Archived from the original
Mass_driver
Plasma device using external magnets to confine plasma
A stellarator is a fusion power device that confines plasma using external magnets. It is one of many types of magnetic confinement fusion devices, and
Stellarator
Conceptual rocket engine
Samuel A. Cohen. It is being modeled and experimentally tested at Princeton Plasma Physics Laboratory, a U.S. Department of Energy facility, as well as modeled
Direct_Fusion_Drive
Proposed spacecraft propulsion method
RAIR consists of three subsystems: a fusion reactor, a scoop field, and a plasma accelerator. Fuel is launched ahead of the ship with the accelerator. The
Bussard_ramjet
Form of electrically powered spacecraft propulsion
resulting from the interaction between the current flowing through the plasma and the magnetic field (which is either externally applied or induced by
Magnetoplasmadynamic_thruster
Type of rocket engine fuel
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Hypergolic_propellant
Rocket that burns 3 propellants at once or 2 fuels with an oxidizer, sequentially
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Tripropellant_rocket
Proposed rocket propulsion mechanism
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Nuclear_salt-water_rocket
Rocket engine operation method
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Staged_combustion_cycle
Type of nuclear propulsion method with an ultra high specific-inpulse
Wyoming, USA. OSTI 6868318. Clark, R.; Sheldon, R. (10–13 July 2005). Dusty Plasma Based Fission Fragment Nuclear Reactor (PDF). 41st AIAA/ASME/SAE/ASEE Joint
Fission-fragment_rocket
Space propulsion system
accelerator grid prevents electrons of the beam plasma outside the thruster from streaming back to the discharge plasma. This can fail due to insufficient negative
Gridded_ion_thruster
Approach to controlled thermonuclear fusion using magnetic fields
coils. Magnet technology is also vital to improving reactor performances, due to the fact that higher magnetic fields result in improved plasma confinement
Magnetic_confinement_fusion
Proposed nuclear pulse propulsion through antimatter-catalyzed nuclear chain reactions
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Antimatter-catalyzed nuclear pulse propulsion
Antimatter-catalyzed_nuclear_pulse_propulsion
Hypothetical spacecraft propulsion through continuous nuclear explosions for thrust
Nuclear pulse propulsion or external pulsed plasma propulsion is a hypothetical method of spacecraft propulsion that uses nuclear explosions for thrust
Nuclear_pulse_propulsion
Rocket with a motor that uses solid propellants
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Solid-propellant_rocket
Electrothermal thruster in development
simplified and compact magnet arrangement in the engine. VASIMR does not use electrodes; instead, it magnetically shields plasma from most hardware parts
Variable Specific Impulse Magnetoplasma Rocket
Variable_Specific_Impulse_Magnetoplasma_Rocket
Spacecraft propulsion technology
developing the intake and the thruster, the latter is the RF helicon-based Plasma Thruster (IPT), which was ignited for the first time in March 2020. Such
Atmosphere-breathing electric propulsion
Atmosphere-breathing_electric_propulsion
Spacecraft propulsion system by NASA. 50kW Hall-effect thrusters, now for Lunar Gateway
system, electrostatic gridded ion thruster VASIMR variable impulse electric plasma engine Overview of the Development and Mission Application of the Advanced
Advanced Electric Propulsion System
Advanced_Electric_Propulsion_System
Type of spacecraft propulsion system
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Nuclear_electric_rocket
Characteristic quantity of plasmas
of fusion power designs. In the fusion power field, plasma is often confined using strong magnets. Since the temperature of the fuel scales with pressure
Plasma_beta
Rocket engine operation method
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Gas-generator_cycle
Propulsion system creating motion without propellant
propellant-based spaceflight or Newtonian mechanics. The Q-thruster, or Quantum Vacuum Plasma Thruster, was a proposed propulsion concept associated with Harold G. White's
Reactionless_drive
Type of rocket engine which uses liquid fuel stored at very low temperatures
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Cryogenic_rocket_engine
Rocket engine operation method
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Expander_cycle
Type of rocket engine
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Cold_gas_thruster
Type of spacecraft propulsion using electrical energy to accelerate propellant
thrusters, and colloid thrusters; electromagnetic devices such as pulsed plasma thrusters, magnetoplasmadynamic thrusters, and pulsed inductive thrusters;
Spacecraft electric propulsion
Spacecraft_electric_propulsion
Device claimed to be a propellantless spacecraft thruster
thrusters could work by transferring momentum to the "quantum vacuum virtual plasma", a new term he coined. Baez and Carroll criticized this explanation, because
EmDrive
Space navigation technique
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Gravity_assist
Nuclear spacecraft propulsion technology
to fusion approaches. The Direct Fusion Drive project at the Princeton Plasma Physics Laboratory is one such example, although "energy-positive fusion
Nuclear_thermal_rocket
Mechanism where confined high-speed particles confer energy to a vehicle
used by an electrically powered rocket engine, such as an ion thruster or plasma propulsion engine. Usually, these schemes assume either solar panels or
Beam-powered_propulsion
Type of solar sail
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Diffractive_solar_sail
Electricity generation by nuclear fusion
Stellarator: Twisted rings of hot plasma. The stellarator attempts to create a natural twisted plasma path, using external magnets. Stellarators were developed
Fusion_power
in orbit around Earth. MagBeam propulsion uses a helicon plasma source to produce a plasma beam. A helicon drive consists of a quartz tube wrapped in
MagBeam
Spacecraft propulsion device
thruster, using ionized air (only for use in an atmosphere) Electrodeless plasma thruster, electric propulsion using ponderomotive force Electrostatic ion
Thrusters_(spacecraft)
Rocket engine that uses liquid fuels and oxidizers
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Liquid-propellant_rocket
Space propulsion system, a gridded electrostatic ion thruster
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
NEXT_(ion_thruster)
Propulsion concepts and technologies
magnetic sails, and electrodynamic tethers, which couple with external photon, plasma, or magnetic fields instead of expelling onboard propellant. Field propulsion
Field_propulsion
Launch system that only uses one rocket stage
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Single-stage-to-orbit
Type of electric spacecraft propulsion system
from the original on 7 July 2011. "FEEP thrusters". Nonequilibrium Gas and Plasma Dynamics Group. University of Michigan. Archived from the original on 21
Field-emission electric propulsion
Field-emission_electric_propulsion
Proposed spacecraft propulsion device
momentum from them. Simultaneously they attract electrons from the solar wind plasma, producing an electron current. The electron gun compensates for the arriving
Electric_sail
Load bearing cable connecting objects in space
including research into tether propulsion, tidal stabilization and orbital plasma dynamics. Five main techniques for employing space tethers are in development:
Space_tether
Class of liquid rocket propellants
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Nitrous_oxide_fuel_blend
Rocket that uses a single propellant with a catalyst
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Monopropellant_rocket
Prototype spacecraft propulsion engine
gas to break down and form a plasma. The antenna then excites a helicon wave in the plasma, which further heats the plasma. The device has a roughly constant
Helicon_double-layer_thruster
Rocket-propelled by exhausted coolant of a gas-cooled nuclear reactor
fission reactor. The nuclear fission reactor core may be either a gas or plasma. They may be capable of creating specific impulses of 3,000–5,000 s (30
Gas_core_reactor_rocket
Rocket engine operation method
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Electric-pump-fed_engine
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Radioisotope_rocket
Spacecraft propulsion using steam as propellant
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
World Is Not Enough (spacecraft propulsion)
World_Is_Not_Enough_(spacecraft_propulsion)
Space propulsion method using Sun radiation
around the wires. The electric field extends a few tens of metres into the plasma of the surrounding solar wind. The solar protons are reflected by the electric
Solar_sail
Method of spacecraft propulsion
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Resistojet_rocket
Theoretical design for a compact fusion reactor
fusion reactor developed by the Massachusetts Institute of Technology (MIT) Plasma Science and Fusion Center (PSFC). ARC aims to achieve an engineering breakeven
ARC_fusion_reactor
Space propulsion system, electrostatic gridded ion thruster
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
NASA Solar Technology Application Readiness
NASA_Solar_Technology_Application_Readiness
Method used to accelerate spacecraft
needed] Plasma propulsion engines Magnetoplasmadynamic thrusters Electrodeless plasma thrusters Pulsed inductive thrusters Pulsed plasma thrusters Variable
Spacecraft_propulsion
Liquid form of rocket propellants
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Liquid_rocket_propellant
Rocket engine that uses photons to propel a spacecraft
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Nuclear_photonic_rocket
Type of spacecraft electric propulsion system
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Arcjet_rocket
International nuclear fusion research and engineering megaproject
absorbed by the plasma) of Q = 10 momentarily and Q = 5 at steady state; to develop fusion power technologies including superconducting magnets, cryogenics
ITER
Form of electric spacecraft propulsion
direction whatever their electric charge, and are specifically referred to as plasma propulsion engines, where the electric field is not in the direction of
Ion_thruster
Type of spacecraft plasma propulsion system
(PIT) is a form of ion thruster, used in spacecraft propulsion. It is a plasma propulsion engine using perpendicular electric and magnetic fields to accelerate
Pulsed_inductive_thruster
Type of space propulsion using microwaves
adjust the spacecraft’s position and orbit. A MET sustains and ignites a plasma in a propellant gas. This creates a heated propellant gas which in turn
Microwave electrothermal thruster
Microwave_electrothermal_thruster
Rocket engine operation method
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Pressure-fed_engine
Extremely light synthetic foam of tubular carbon molecules
lightspeed or 6000 km/sec. A steady stream of pellets could be used by plasma magnet propulsion systems to accelerate payloads to 6% of lightspeed, or 18000
Aerographite
Hypothetical type of spacecraft
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Nuclear_lightbulb
Laboratory in Princeton, New Jersey, United States
The Princeton Plasma Physics Laboratory (PPPL) is a United States Department of Energy national laboratory for plasma physics and nuclear fusion science
Princeton Plasma Physics Laboratory
Princeton_Plasma_Physics_Laboratory
Type of nuclear thermal rocket
the order of 1 kHz to 10 kHz are likely choices. Fission fragment rocket Plasma propulsion engine Arias, Francisco. J (2016). "On the Use of a Pulsed Nuclear
Pulsed_nuclear_thermal_rocket
Rocket engine power cycle
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Combustion_tap-off_cycle
Theoretical spacecraft propulsion system
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Solar_thermal_rocket
electrodes to produce thrust. A metal plasma is produced from micrometer-size cathodic spots and the momentum from the plasma creates thrust for the vacuum arc
Vacuum_arc_thruster
Monopropellant
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Cavea-B
microwave to the electrons. This energy is then transferred to the bulk gas/plasma via the rare - yet important - collisions between electrons and neutrals
High Power Electric Propulsion
High_Power_Electric_Propulsion
Rocket engine that uses both liquid / gaseous and solid fuel
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Hybrid-propellant_rocket
Hypothetical method of spacecraft propulsion
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Fission_sail
Concept of permanent human habitation outside of Earth
Jupiter in a reasonable amount of time. Another possibility would be plasma magnet sails, a technology already suggested for rapidly sending a probe to
Space_colonization
US spacecraft
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
CubeSail_(UltraSail)
Ion thruster subtype
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
Colloid_thruster
Ferrimagnetic ceramic material
attracted by magnetic fields and can be magnetized to become permanent magnets. Unlike many ferromagnetic materials, most ferrites are not electrically-conductive
Ferrite_(magnet)
Traumatically caused infection in animals, usually cattle
conclusively diagnose, but can be prevented by the oral administration of a magnet around the time that the animal reaches the age of one year. Depending on
Hardware_disease
type of plasmoid, a class of toroidal plasma configuration that is self-stable, and which does not need magnet coils running through the center of the
Compact_toroid
Industrial process
Plasma etching is a form of plasma processing used to fabricate integrated circuits. It involves a high-speed stream of glow discharge (plasma) of an appropriate
Plasma_etching
Plasma whose heat comes from fusion reactions
In plasma physics, a burning plasma is a plasma that is heated primarily by fusion reactions involving thermal plasma ions. The Sun and similar stars are
Burning_plasma
Type of mass spectrometry that uses an inductively coupled plasma to ionize the sample
Inductively coupled plasma mass spectrometry (ICP-MS) is a type of mass spectrometry that uses an inductively coupled plasma to ionize the sample. It atomizes
Inductively coupled plasma mass spectrometry
Inductively_coupled_plasma_mass_spectrometry
Study of space plasmas in the Solar System
Space physics, also known as space plasma physics, is the study of naturally occurring plasmas within Earth's upper atmosphere and the rest of the Solar
Space_physics
Fusion power experiment
plasma on Friday, August 13, 2004, at 12:53 PM. First plasma was done by (1) successfully levitating the dipole magnet and (2) RF heating the plasma.
Levitated_Dipole_Experiment
Research apparatus for particle physics
functions can be separated. Instead of one huge magnet, one has a line of hundreds of bending magnets, enclosing (or enclosed by) vacuum connecting pipes
Particle_accelerator
In plasma astrophysics, the corotation electric field is the electric field due to the rotation of a magnet. For example, the rotation of the Earth results
Corotation_electric_field
Forms which matter can take
states of matter are observable in everyday life: solid, liquid, gas, and plasma. Different states are distinguished by the ways the component particles
State_of_matter
Experimental fusion reactor
high-temperature superconducting magnets that retain superconductivity at temperatures as high as 77 K (optimally at 10 K). The resulting plasmas are expected to generate
SPARC_(tokamak)
American nuclear fusion and energy company
labs and universities. CFS was founded in 2018 as a spin-off from the MIT Plasma Science and Fusion Center. After initial funding of $50 million in 2018
Commonwealth_Fusion_Systems
thruster Magnetoplasmadynamic thruster Electrodeless plasma thruster Plasma magnet Electrothermal Pulsed plasma thruster Vacuum arc thruster Helicon double-layer
List of spacecraft with electric propulsion
List_of_spacecraft_with_electric_propulsion
Plasma Physics Experiment
The Star Thrust Experiment (STX) was a plasma physics experiment at the University of Washington's Redmond Plasma Physics Laboratory which ran from 1999
Star_Thrust_Experiment
New Zealand nuclear fusion company
Marsden, and its first magnet inside is named Junior. The vacuum chamber (Marsden) diameter is about 5 metres (16 ft); the magnet (Junior) diameter is about
OpenStar
PLASMA MAGNET
PLASMA MAGNET
Girl/Female
Arabic
Variant of Ma'sma; Innocent; Infallible
Boy/Male
Hindu, Indian
A Mark of Love
Male
Native American
Native American Dakota name MAZA BLASKA means "flat iron."
Boy/Male
Muslim
Pasha. A Title.
Male
Russian
(Паша) Russian pet form of Czech/Russian Pavel, PASHA means "small."
Girl/Female
Spanish American
Dove.
Female
Hebrew
Variant spelling of Hebrew Bosma, BASMA means perfumed."
Girl/Female
Latin
Stammers.
Boy/Male
Indian, Sanskrit
Ash
Girl/Female
American, Australian, Latin
Dove; Abbreviation of Paloma
Girl/Female
Hindu, Indian
God Name
Female
Spanish
Spanish name PALOMA means "dove, pigeon."
Girl/Female
Muslim
Sky, Excellent, Precious
Girl/Female
Hindu
Female
Hindi/Indian
(पदà¥à¤®) Hindi unisex name PADMA means "lotus flower."
Girl/Female
Hindu, Indian, Tamil
Love; A Mark of Love
Surname or Lastname
North German
North German : topographic name from Middle Low German plas ‘place’, ‘open square’, ‘street’.South German (also Pläss) : from a short form of the medieval personal name Blasius.English : variant of Place 3.
Male
Czechoslovakian
, power.
Boy/Male
Hindu, Indian
White Dove
Girl/Female
Gujarati, Hindu, Indian, Kannada
Goddess Saraswati
PLASMA MAGNET
PLASMA MAGNET
PLASMA MAGNET
PLASMA MAGNET
PLASMA MAGNET
PLASMA MAGNET
PLASMA MAGNET