2000
DOI: 10.1255/ejms.379
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Ideal Space Focusing in a Time-of-Flight Mass Spectrometer: An Optimization Using an Analytical Approach

Abstract: An exact, analytical solution for an electric field in a nonlinear acceleration region of an ion source for the cases of linear and reflectron time-of-flight (TOF) mass spectrometers has been found to achieve universal temporal focusing of ions having an initial space distribution. The general solutions are valid for an arbitrary electric field distribution in the drift region (from the ion source to an ion detector) of a linear TOF mass spectrometer, and in the upstream (from the ion source to the reflectron)… Show more

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Cited by 3 publications
(3 citation statements)
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“…A method similar to that described by Managadze et al (), was used to solve equations for the total flight time of an ion in an ion mirror. Later, a similar approach for space focusing in linear and ion mirror TOF was introduced by Doroshenko (). A general solution was presented for one‐ and two‐stage acceleration in both the case of a linear TOF and the case of an ion mirror.…”
Section: Ion Mirrors In Time‐of‐flightmentioning
confidence: 99%
See 1 more Smart Citation
“…A method similar to that described by Managadze et al (), was used to solve equations for the total flight time of an ion in an ion mirror. Later, a similar approach for space focusing in linear and ion mirror TOF was introduced by Doroshenko (). A general solution was presented for one‐ and two‐stage acceleration in both the case of a linear TOF and the case of an ion mirror.…”
Section: Ion Mirrors In Time‐of‐flightmentioning
confidence: 99%
“…Yoshida (1986) and Andersen et al (1998) explored so-called quadraticfield ion mirrors in various TOFs and tandem TOFs. The socalled curved-field ion mirror was promoted by Cotter and also Doroshenko (Doroshenko & Cotter, 1999;Doroshenko, 2000). Constant momentum TOF was developed by Santacruz et al (2006).…”
Section: Overview Of the Historymentioning
confidence: 99%
“…The last missing bit is the time spent in the post-acceleration gap, d p of Figure 3, which is again calculated using Equations (16), (17) and 22: Now we have all the parts to build the time-of-flight equation for the whole instrument. The derived formulae are exact for any instrument that uses homogeneous electric fields.…”
Section: Nomenclature and Basic Formulaementioning
confidence: 99%