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Related Concept Videos

Inductively Coupled Plasma–Mass Spectrometry (ICP–MS): Overview01:19

Inductively Coupled Plasma–Mass Spectrometry (ICP–MS): Overview

In inductively coupled plasma–mass spectrometry (ICP–MS), an inductively coupled plasma (ICP) torch is used as an atomizer and ionizer. Solid samples are dissolved and volatilized before being introduced into the high-temperature argon plasma, while solution samples are nebulized and passed through the high-temperature argon plasma. Plasma dissociates the analytes and ionizes their component atoms to form a mixture of positive ions and molecular species. The positive ions are then passed on to...
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Inductively coupled plasma (ICP) is the most widely used plasma source in atomic emission spectroscopy (AES), also known as Inductively Coupled Plasma Optical Emission Spectroscopy (ICP-OES). The ICP source, or torch, consists of three concentric quartz tubes with argon gas flowing through them. A spark from a Tesla coil initiates the ionization of argon, generating a high-temperature plasma.
The ions and electrons produced interact with the fluctuating magnetic field created by a water-cooled...
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Inductively coupled plasma (ICP) is the common plasma source used in atomic emission spectroscopy (AES), a technique that detects and analyzes various elements in a sample. This method is often called inductively coupled plasma atomic emission spectroscopy (ICP-AES).
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Updated: May 12, 2026

Non-equilibrium Microwave Plasma for Efficient High Temperature Chemistry
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A microwave interferometer for small and tenuous plasma density measurements.

O Tudisco1, A Lucca Fabris, C Falcetta

  • 1ENEA CR Frascati, Via E. Fermi 45, 00044 Frascati, Italy. onofrio.tudisco@enea.it

The Review of Scientific Instruments
|April 6, 2013
PubMed
Summary

A new microwave interferometer enables non-intrusive plasma density measurement for space thrusters. This high-sensitivity device accurately measures low densities, crucial for understanding mini-helicon thruster performance.

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Area of Science:

  • Plasma physics
  • Space propulsion engineering

Background:

  • Non-intrusive plasma density measurement is challenging for small, high-density sources.
  • Mini-helicon space thrusters produce thin plasmas with densities ranging from 10^16 to 10^19 m^-3.

Purpose of the Study:

  • To develop a non-intrusive method for measuring plasma density in a mini-helicon space thruster.
  • To overcome the challenges posed by the broad density range and small source size.

Main Methods:

  • Development of a microwave interferometer with a small probing beam wavelength (λ = 4 mm).
  • Utilization of a low-noise digital phase detector with a phase noise of 0.02°.

Main Results:

  • The developed interferometer achieves high sensitivity, capable of detecting densities as low as 0.5 × 10^16 m^-3.
  • Successful non-intrusive density measurement within the specified range for the mini-helicon thruster.

Conclusions:

  • The microwave interferometer is a viable tool for non-intrusive plasma density diagnostics in small space thrusters.
  • The high sensitivity achieved is critical for characterizing low-density plasma regimes in such devices.