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The Hall Effect01:30

The Hall Effect

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Edwin H. Hall, in the year 1879, devised an experiment that could be used to identify the polarity of the predominant charge carriers in a conducting material. From a historical perspective, this experiment was the first to demonstrate that the charge carriers in most metals are negative.
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Maximum Power Transfer01:16

Maximum Power Transfer

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Numerous practical applications within engineering disciplines, such as telecommunications, necessitate optimizing power delivery to a connected load. This pursuit, however, entails inherent internal losses, which can either equal or exceed the power supplied to the load. The Thevenin equivalent circuit is helpful in finding the maximum power a linear circuit can deliver to a load. It is assumed in this context that the load resistance can be adjusted.
By substituting the entire circuit with...
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Rocket Propulsion in Gravitational Field - II01:03

Rocket Propulsion in Gravitational Field - II

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A rocket's velocity in the presence of a gravitational field is decreased by the amount of force exerted by Earth's gravitational field, which opposes the motion of the rocket. If we consider thrust, that is, the force exerted on a rocket by the exhaust gases, then a rocket's thrust is greater in outer space than in the atmosphere or on a launch pad. In fact, gases are easier to expel in a vacuum.
A rocket's acceleration depends on three major factors, consistent with the...
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Faraday Disk Dynamo01:23

Faraday Disk Dynamo

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A Faraday disk dynamo is a DC generator, producing an emf that is constant in time. It consists of a conducting disk that rotates with a constant angular velocity in the magnetic field, perpendicular to the disk's plane. The rotation of the disk causes a change in magnetic flux, which induces an emf, causing opposite charges to develop on the rim and in the center of the disk. The polarity of the induced emf can be determined by the direction of the magnetic field and the direction of the...
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Rocket Propulsion in Gravitational Field - I01:20

Rocket Propulsion in Gravitational Field - I

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Rockets range in size from small fireworks that ordinary people use to the enormous Saturn V that once propelled massive payloads toward the Moon. The propulsion of all rockets, jet engines, deflating balloons, and even squids and octopuses are explained by the same physical principle: Newton's third law of motion. The matter is forcefully ejected from a system, producing an equal and opposite reaction on what remains.
The motion of a rocket in space changes its velocity (and hence its...
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Torque On A Current Loop In A Magnetic Field01:13

Torque On A Current Loop In A Magnetic Field

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The most common application of magnetic force on current-carrying wires is in electric motors. These consist of loops of wire, which are placed between the magnets with a magnetic field. When current flows through the loops, the magnetic field applies torque, which causes the shaft to rotate, thus converting electrical energy to mechanical energy.
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Related Experiment Video

Updated: May 17, 2025

Optimization, Test and Diagnostics of Miniaturized Hall Thrusters
12:22

Optimization, Test and Diagnostics of Miniaturized Hall Thrusters

Published on: February 16, 2019

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The H10 high power density hall thruster.

Richard R Hofer1, Jacob B Simmonds1, Dan M Goebel1

  • 1Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA USA.

Journal of Electric Propulsion
|May 16, 2025
PubMed
Summary
This summary is machine-generated.

JPL developed a new Hall thruster (H10) achieving 3,000 s specific impulse for deep-space missions. This high-power density thruster significantly enhances propulsion capabilities for robotic and human exploration.

Keywords:
Graphite discharge chamberHall thrusterHigh power densityLaB6 hollow cathodeMagnetic shieldingThermal management

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Area of Science:

  • Aerospace Engineering
  • Plasma Physics
  • Electric Propulsion

Background:

  • Magnetic shielding has increased Hall thruster lifespan for deep-space missions.
  • Current Hall thrusters have specific impulses < 2,000 s, limiting high-velocity change missions.
  • Higher specific impulses (> 3,000 s) are needed for broader mission applications.

Purpose of the Study:

  • Develop a low-mass, 10-kW class Hall thruster with > 3,000 s specific impulse.
  • Achieve wide power throttling ratios for versatile deep-space propulsion.
  • Demonstrate high power density operation exceeding the state-of-the-art.

Main Methods:

  • Developed the H10 Hall thruster with an integrated, conducting wall, magnetically shielded discharge chamber.
  • Implemented a passive, multi-zone heat rejection system for high power density.
  • Conducted performance testing at various power levels and voltages.

Main Results:

  • Demonstrated 2:1 power throttling at 800 V (~3,000 s specific impulse).
  • Achieved efficiencies > 50% over 6:1 power throttling.
  • Reached peak performance of 457 mN thrust, 3400 s specific impulse, and 76% efficiency at 800 V, 10 kW.
  • Demonstrated 50:1 power throttling over 0.2-10 kW and thermal steady-state at 15 kW.

Conclusions:

  • The H10 Hall thruster represents a new class of high-power density electric propulsion.
  • This technology enables next-generation robotic science and human exploration missions.
  • The thruster's performance characteristics significantly expand mission capabilities for deep-space exploration.