Electrostatic analyzer

Last updated

An electrostatic analyzer or ESA is an instrument used in ion optics that employs an electric field to allow the passage of only those ions or electrons that have a given specific energy. It usually also focuses these particles (concentrates them) into a smaller area. ESAs are typically used as components of space instrumentation, to limit the scanning (sensing) energy range and, thereby also, the range of particles targeted for detection and scientific measurement. The closest analogue in photon optics is a filter.

Contents

Radial cylindrical analyzer

Electrostatic analyzers are designed in different configurations. A simple version is a radial cylindrical analyzer, which consists of two curved parallel plates at different potentials. Ions or electrons enter the analyzer at one end and either pass through the other end or collide with the walls of the analyzer, depending on their initial energy. In these types of analyzers, only the radial component of the velocity of a charged particle is changed by an ESA since the potential on the plates only varies in the radial direction if one considers the geometry in cylindrical coordinates. Poisson's Equation can be then used to calculate the magnitude of the electric field pointing radially inwards. The resultant inward-pointing force generated by this electric field will cause the particles' trajectories to curve in a uniform circular motion. Depending on initial energy (velocity), only certain particles will therefore have the "correct" motion to exit the analyzer by tracing its physical structure, while others will collide into the walls of the instrument. In addition to the energy, the angle of entry will also affect the particles' time-of-flight through the analyzer as well as exit angle. In practice, the plates are usually oppositely charged and at very high potentials. Also, the inner surface of the analyzer, usually made of aluminum for space missions, is sometimes plated with black chrome or even Ebonol C to absorb stray light, instead of allowing it to bounce its way through.

Face-field cylindrical and conical electrostatic energy analyzers

The well-known class of cylindrical face-field energy analyzers and a more recently developed type of face-field conical electrostatic energy analyzers are very useful instruments with very wide area of applications. These instruments can achieve very high energy resolution combined with large acceptance aperture, what is very important for measurements of in-space plasma flows. [1] [2] This new class of analyzers can be used in a variety of applications for studying objects with different forms and sizes, [3] and for analysis of remote objects in the exploration of nanomaterials within a set of different methods. [4]

ESAs are usually designed and analyzed using an off-the-shelf ion-optics simulation-software package which includes the capability of performing Monte Carlo simulations on known test particles, thus providing the designer a better understanding of the response characteristics of the analyzer itself.

Use in space instrumentation

Examples of space instruments or missions using Electrostatic Analyzers:

See also

Related Research Articles

<i>Nozomi</i> (spacecraft) Failed Mars orbiter

Nozomi was a Japanese Mars orbiter that failed to reach Mars due to electrical failure. It was constructed by the Institute of Space and Astronautical Science, University of Tokyo and launched on July 4, 1998, at 03:12 JST with an on-orbit dry mass of 258 kg and 282 kg of propellant. The Nozomi mission was terminated on December 31, 2003.

<span class="mw-page-title-main">Advanced Composition Explorer</span> NASA satellite of the Explorer program, at SE-L1, studying solar wind etc

Advanced Composition Explorer is a NASA Explorer program satellite and space exploration mission to study matter comprising energetic particles from the solar wind, the interplanetary medium, and other sources.

<i>Wind</i> (spacecraft) NASA probe to study solar wind, at L1 since 1995

The Global Geospace Science (GGS) Wind satellite is a NASA science spacecraft designed to study radio waves and plasma that occur in the solar wind and in the Earth's magnetosphere. It was launched on 1 November 1994, at 09:31:00 UTC, from launch pad LC-17B at Cape Canaveral Air Force Station (CCAFS) in Merritt Island, Florida, aboard a McDonnell Douglas Delta II 7925-10 rocket. Wind was designed and manufactured by Martin Marietta Astro Space Division in East Windsor Township, New Jersey. The satellite is a spin-stabilized cylindrical satellite with a diameter of 2.4 m and a height of 1.8 m.

<span class="mw-page-title-main">Fast Auroral SnapshoT Explorer</span> NASA satellite of the Explorer program

The Fast Auroral SnapshoT Explorer was a NASA plasma physics satellite, and was the second spacecraft in the Small Explorer program (SMEX). It was launched on 21 August 1996, from Vandenberg Air Force Base aboard a Pegasus XL launch vehicle. The spacecraft was designed and built by NASA's Goddard Space Flight Center (GSFC). Flight operations were handled by GSFC for the first three years, and thereafter were transferred to the University of California, Berkeley's Space Sciences Laboratory.

<span class="mw-page-title-main">Magnetospheric Multiscale Mission</span> Four NASA robots studying Earths magnetosphere (2015-present)

The Magnetospheric Multiscale (MMS) Mission is a NASA robotic space mission to study the Earth's magnetosphere, using four identical spacecraft flying in a tetrahedral formation. The spacecraft were launched on 13 March 2015 at 02:44 UTC. The mission is designed to gather information about the microphysics of magnetic reconnection, energetic particle acceleration, and turbulence⁠ — processes that occur in many astrophysical plasmas. As of March 2020, the MMS spacecraft have enough fuel to remain operational until 2040.

<span class="mw-page-title-main">Explorer 54</span> NASA satellite of the Explorer program

Explorer 54, also called as AE-D, was a NASA scientific satellite belonging to series Atmosphere Explorer, being launched on 6 October 1975 from Vandenberg Air Force Base board a Thor-Delta 2910 launch vehicle.

<span class="mw-page-title-main">Energetic neutral atom</span> Technology to create global images of otherwise invisible phenomena

Energetic Neutral Atom (ENA) imaging is a technology used to create global images of otherwise invisible phenomena in the magnetospheres of planets and throughout the heliosphere.

<span class="mw-page-title-main">ISEE-1</span> NASA satellite of the Explorer program

The ISEE-1 was an Explorer-class mother spacecraft, International Sun-Earth Explorer-1, was part of the mother/daughter/heliocentric mission. ISEE-1 was a 340.2 kg (750 lb) space probe used to study magnetic fields near the Earth. ISEE-1 was a spin-stabilized spacecraft and based on the design of the prior IMP series of spacecraft. ISEE-1 and ISEE-2 were launched on 22 October 1977, and they re-entered on 26 September 1987.

<span class="mw-page-title-main">ISEE-2</span>

The ISEE-2 was an Explorer-class daughter spacecraft, International Sun-Earth Explorer-2, was part of the mother/daughter/heliocentric mission. ISEE-2 was a 165.78 kg (365.5 lb) space probe used to study magnetic fields near the Earth. ISEE-2 was a spin-stabilized spacecraft and based on the design of the prior IMP series of spacecraft. ISEE-1 and ISEE-2 were launched on 22 October 1977, and they re-entered on 26 September 1987.

<span class="mw-page-title-main">Explorer 43</span> NASA satellite of the Explorer program

Explorer 43, also called as IMP-I and IMP-6, was a NASA satellite launched as part of Explorer program. Explorer 43 was launched on 13 March 1971 from Cape Canaveral Air Force Station (CCAFS), with a Thor-Delta M6 launch vehicle. Explorer 43 was the sixth satellite of the Interplanetary Monitoring Platform.

<span class="mw-page-title-main">Explorer 45</span> NASA satellite of the Explorer program

Explorer 45 was a NASA satellite launched as part of Explorer program. Explorer 45 was the only one to be released from the program Small Scientific Satellite.

<span class="mw-page-title-main">Explorer 47</span> NASA satellite of the Explorer program

Explorer 47, was a NASA satellite launched as part of Explorer program. Explorer 47 was launched on 23 September 1972 from Cape Canaveral, Florida, with a Thor-Delta 1604. Explorer 47 was the ninth overall launch of the Interplanetary Monitoring Platform series, but received the launch designation "IMP-7" because two previous "Anchored IMP" flights had used "AIMP" instead.

<span class="mw-page-title-main">Explorer 50</span> NASA satellite of the Explorer program

Explorer 50, also known as IMP-J or IMP-8, was a NASA satellite launched to study the magnetosphere. It was the eighth and last in a series of the Interplanetary Monitoring Platform.

<span class="mw-page-title-main">Explorer 51</span> NASA satellite of the Explorer program

Explorer 51, also called as AE-C, was a NASA scientific satellite belonging to series Atmosphere Explorer, being launched on 16 December 1973, at 06:18:00 UTC, from Vandenberg board a Delta 1900 launch vehicle.

<span class="mw-page-title-main">Explorer 55</span> NASA satellite of the Explorer program

Explorer 55, also called as AE-E, was a NASA scientific satellite belonging to series Atmosphere Explorer, being launched on 20 November 1975 from Cape Canaveral Air Force Station (CCAFS) board a Thor-Delta 2910 launch vehicle.

<span class="mw-page-title-main">AMPTE-CCE</span> NASA satellite of the Explorer program

AMPTE-Charge Composition Explorer, also called as AMPTE-CCE or Explorer 65, was a NASA satellite designed and tasked to study the magnetosphere of Earth, being launched as part of the Explorer program. The AMPTE mission was designed to study the access of solar wind ions to the magnetosphere, the convective-diffusive transport and energization of magnetospheric particles, and the interactions of plasmas in space.

<span class="mw-page-title-main">Dynamics Explorer 1</span> NASA satellite of the Explorer program

Dynamics Explorer 1 was a NASA high-altitude mission, launched on 3 August 1981, and terminated on 28 February 1991. It consisted of two satellites, DE-1 and DE-2, whose purpose was to investigate the interactions between plasmas in the magnetosphere and those in the ionosphere. The two satellites were launched together into polar coplanar orbits, which allowed them to simultaneously observe the upper and lower parts of the atmosphere.

<span class="mw-page-title-main">Dynamics Explorer 2</span> NASA satellite of the Explorer program

Dynamics Explorer 2 was a NASA low-altitude mission, launched on 3 August 1981. It consisted of two satellites, DE-1 and DE-2, whose purpose was to investigate the interactions between plasmas in the magnetosphere and those in the ionosphere. The two satellites were launched together into polar coplanar orbits, which allowed them to simultaneously observe the upper and lower parts of the atmosphere.

AMPTE-IRM, also called as AMPTE-Ion Release Module, was a Germany satellite designed and tasked to study the magnetosphere of Earth, being launched as part of the Explorer program. The AMPTE mission was designed to study the access of solar wind ions to the magnetosphere, the convective-diffusive transport and energization of magnetospheric particles, and the interactions of plasmas in space.

AMPTE-UKS, also called as AMPTE-United Kingdom Subsatellite, was a United Kingdom satellite designed and tasked to study the magnetosphere of Earth, being launched as part of the Explorer program. The AMPTE mission was designed to study the access of solar wind ions to the magnetosphere, the convective-diffusive transport and energization of magnetospheric particles, and the interactions of plasmas in space.

References

  1. Ilyin, A. M. (2003). "New class of electrostatic energy analyzers with a cylindrical face-field". Nuclear Instruments and Methods in Physics Research Section A. 500 (1–3): 62–67. Bibcode:2003NIMPA.500...62I. doi:10.1016/S0168-9002(03)00334-6.
  2. Ilyin, A. M.; Ilyina, I. A. (2005). "New electrostatic energy analysers with a bounded cylindrical field". Measurement Science and Technology. 16 (9): 1798–1801. Bibcode:2005MeScT..16.1798I. doi:10.1088/0957-0233/16/9/012. ISSN   0957-0233. S2CID   121955696.
  3. Ilyin, A. M. and I. A. Ilyina (2007). "An electrostatic face-field energy analyzer for space and plasma measurements". Measurement Science and Technology. 18 (3): 724–726. Bibcode:2007MeScT..18..724I. doi:10.1088/0957-0233/18/3/023. S2CID   121520374.
  4. Ilyin, A. M.; N. R. Guseinov; M. A. Tulegenova (2022). "Conical Face-Field electrostatic energy analyzers for investigating nanomaterials". J. Electr. Spectr. Relat. Phenom. 257.
  5. Barabash, S.; Lundin, R.; Andersson, H.; Brinkfeldt, K.; Grigoriev, A.; Gunell, H.; Holmström, M.; Yamauchi, M.; Asamura, K.; Bochsler, P.; Wurz, P.; Cerulli-Irelli, R.; Mura, A.; Milillo, A.; Maggi, M.; Orsini, S.; Coates, A. J.; Linder, D. R.; Kataria, D. O.; Curtis, C. C.; Hsieh, K. C.; Sandel, B. R.; Frahm, R. A.; Sharber, J. R.; Winningham, J. D.; Grande, M.; Kallio, E.; Koskinen, H.; Riihelä, P.; et al. (2007). "The Analyzer of Space Plasmas and Energetic Atoms (ASPERA-3) for the Mars Express Mission". Space Science Reviews. 126 (1–4): 113–164. doi:10.1007/s11214-006-9124-8. S2CID   189767397.
  6. "Orbiter Instruments". sci.esa.int. Retrieved 2019-06-26.