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magnetop

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The answer MAGNETOP has 0 possible clue(s) in existing crosswords.

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The word MAGNETOP is NOT valid in any word game. (Sorry, you cannot play MAGNETOP in Scrabble, Words With Friends etc)

There are 8 letters in MAGNETOP ( A¹E¹G²M³N¹O¹P³T¹ )

To search all scrabble anagrams of MAGNETOP, to go: MAGNETOP?

Rearrange the letters in MAGNETOP and see some winning combinations

4 letters out of MAGNETOP

3 letters out of MAGNETOP

AGE AGO AMP ANE ANT APE APO APT ATE EAT EGO ENG EON ETA GAE GAM GAN GAP GAT GEM GEN GET GOA GOT MAE MAG MAN MAP MAT MEG MEN MET MOA MOG MON MOP MOT NAE NAG NAM NAP NEG NET NOG NOM NOT OAT ONE OPE OPT PAM PAN PAT PEA PEG PEN PET POM POT TAE TAG TAM TAN TAO TAP TEA TEG TEN TOE TOG TOM TON TOP

2 letters out of MAGNETOP

AE AG AM AN AT EM EN ET GO MA ME MO NA NE NO OE OM ON OP PA PE TA TO

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Definitions of magnetop in various dictionaries:

MAGNETOP - A magnetoplasmadynamic (MPD) thruster (MPDT) is a form of electrically powered spacecraft propulsion which uses the Lorentz force (the force on a cha...

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Magnetop might refer to
A magnetoplasmadynamic (MPD) thruster (MPDT) is a form of electrically powered spacecraft propulsion which uses the Lorentz force (the force on a charged particle by an electromagnetic field) to generate thrust. It is sometimes referred to as Lorentz Force Accelerator (LFA) or (mostly in Japan) MPD arcjet. * Generally, a gaseous material is ionized and fed into an acceleration chamber, where the magnetic and electrical fields are created using a power source. The particles are then propelled by the Lorentz force resulting from the interaction between the current flowing through the plasma and the magnetic field (which is either externally applied, or induced by the current) out through the exhaust chamber. Unlike chemical propulsion, there is no combustion of fuel. As with other electric propulsion variations, both specific impulse and thrust increase with power input, while thrust per watt drops. * There are two main types of MPD thrusters, applied-field and self-field. Applied-field thrusters have magnetic rings surrounding the exhaust chamber to produce the magnetic field, while self-field thrusters have a cathode extending through the middle of the chamber. Applied fields are necessary at lower power levels, where self-field configurations are too weak. Various propellants such as xenon, neon, argon, hydrogen, hydrazine, and lithium have been used, with lithium generally being the best performer. * According to Edgar Choueiri magnetoplasmadynamic thrusters have input power 100–500 kilowatts, exhaust velocity 15–60 kilometers per second, thrust 2.5–25 newtons and efficiency 40–60 percent.One potential application of magnetoplasmadynamic thrusters is the main propulsion engine for heavy cargo and piloted space vehicles (example engine * * * * * a * * 2 * * * * * {\displaystyle a^{2}} * for Manned mission to Mars).

Magnetop might refer to

A magnetoplasmadynamic (MPD) thruster (MPDT) is a form of electrically powered spacecraft propulsion which uses the Lorentz force (the force on a charged particle by an electromagnetic field) to generate thrust. It is sometimes referred to as Lorentz Force Accelerator (LFA) or (mostly in Japan) MPD arcjet.
* Generally, a gaseous material is ionized and fed into an acceleration chamber, where the magnetic and electrical fields are created using a power source. The particles are then propelled by the Lorentz force resulting from the interaction between the current flowing through the plasma and the magnetic field (which is either externally applied, or induced by the current) out through the exhaust chamber. Unlike chemical propulsion, there is no combustion of fuel. As with other electric propulsion variations, both specific impulse and thrust increase with power input, while thrust per watt drops.
* There are two main types of MPD thrusters, applied-field and self-field. Applied-field thrusters have magnetic rings surrounding the exhaust chamber to produce the magnetic field, while self-field thrusters have a cathode extending through the middle of the chamber. Applied fields are necessary at lower power levels, where self-field configurations are too weak. Various propellants such as xenon, neon, argon, hydrogen, hydrazine, and lithium have been used, with lithium generally being the best performer.
* According to Edgar Choueiri magnetoplasmadynamic thrusters have input power 100–500 kilowatts, exhaust velocity 15–60 kilometers per second, thrust 2.5–25 newtons and efficiency 40–60 percent.One potential application of magnetoplasmadynamic thrusters is the main propulsion engine for heavy cargo and piloted space vehicles (example engine
*
*
*
*
* a
*
* 2
*
*
*
*
* {\displaystyle a^{2}}
* for Manned mission to Mars).

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