scholarly journals Experimental Validation of an Ion Beam Optics Code with a Visualized Ion Thruster

2009 ◽  
Vol 57 (662) ◽  
pp. 117-123 ◽  
Author(s):  
Yoshinori NAKAYAMA ◽  
Masakatsu NAKANO
Instruments ◽  
2021 ◽  
Vol 5 (1) ◽  
pp. 10
Author(s):  
Sören Möller ◽  
Daniel Höschen ◽  
Sina Kurth ◽  
Gerwin Esser ◽  
Albert Hiller ◽  
...  

The analysis of material composition by ion-beam analysis (IBA) is becoming a standard method, similar to electron microscopy. A pool of IBA methods exists, from which the combination of particle-induced-X-ray emission (PIXE), particle induced gamma-ray analysis (PIGE), nuclear-reaction-analysis (NRA), and Rutherford-backscattering-spectrometry (RBS) provides the most complete analysis over the whole periodic table in a single measurement. Yet, for a highly resolved and accurate IBA analysis, a sophisticated technical setup is required integrating the detectors, beam optics, and sample arrangement. A new end-station developed and installed in Forschungszentrum Jülich provides these capabilities in combination with high sample throughput and result accuracy. Mechanical tolerances limit the device accuracy to 3% for RBS. Continuous pumping enables 5*10−8 mbar base pressure with vibration amplitudes < 0.1 µm. The beam optics achieves a demagnification of 24–34, suitable for µ-beam analysis. An in-vacuum manipulator enables scanning 50 × 50 mm² sample areas with 10 nm accuracy. The setup features the above-mentioned IBA detectors, enabling a broad range of analysis applications such as the operando analysis of batteries or the post-mortem analysis of plasma-exposed samples with up to 3000 discrete points per day. Custom apertures and energy resolutions down to 11 keV enable separation of Fe and Cr in RBS. This work presents the technical solutions together with the quantification of these challenges and their success in the form of a technical reference.


2020 ◽  
Vol 36 (2) ◽  
pp. 202-210 ◽  
Author(s):  
M. Dobkevicius ◽  
D. Feili ◽  
M. Smirnova ◽  
A. M. Perez

Radiocarbon ◽  
1997 ◽  
Vol 40 (1) ◽  
pp. 247-253 ◽  
Author(s):  
Karl F. Von Reden ◽  
Ann P. McNichol ◽  
Ann Pearson ◽  
Robert J. Schneider

The NOSAMS facility at Woods Hole Oceanographic Institution has started to develop and apply techniques for measuring very small samples on a standard Tandetron accelerator mass spectrometry (AMS) system with high-current hemispherical Cs sputter ion sources. Over the past year, results on samples ranging from 7 to 160 μg C showed both the feasibility of such analyses and the present limitations on reducing the size of solid carbon samples. One of the main factors affecting the AMS results is the dependence of a number of the beam optics parameters on the extracted ion beam current. The extracted currents range from 0.5 to 10 μA of 12C− for the sample sizes given above. We here discuss the setup of the AMS system and methods for reliable small-sample measurements and give the AMS-related limits to sample size and the measurement uncertainties.


Vacuum ◽  
1989 ◽  
Vol 39 (11-12) ◽  
pp. 1043-1046 ◽  
Author(s):  
Peter Spädtke ◽  
Detlef Ivens
Keyword(s):  
Ion Beam ◽  

2018 ◽  
Vol 122 (1255) ◽  
pp. 1425-1441 ◽  
Author(s):  
C. Lu ◽  
P. Qiu ◽  
Y. Cao ◽  
T.P. Zhang ◽  
J.J. Chen

ABSTRACTCharge Exchange (CEX) ion is the main factor causing the plume pollution. The distribution of CEX ions is determined by the distribution of beam ions and neutral atoms. Hence, the primary problem in the study of the plume is how to accurately simulate the distribution of beam ions and neutral atoms. At present, the most commonly used model utilised for the plume simulation is the analytical model proposed by Roy for the plume simulation of the NASA Solar Technology Application Readiness (NSTAR) ion thruster. However, this analytical model can only be applied to the ion beam with small divergence angles. In addition, the analytical model is no longer applicable to the simulation for the plume of a new type of ion thruster that appeared recently, which is called the annular ion thruster. In this paper, a 3D particle model is proposed for the plume simulation of ion thrusters consisting of the particle model for beam ions, the Direct Simulation Monte Carlo (DSMC) model for neutral atoms and the Immersed Finite Element-Particle In Cell-Monte Carlo Collision (IFE-PIC-MCC) model for CEX ions. Then, the plume of the NSTAR ion thruster is simulated by both Roy's model and the 3D particle model. The simulation results of both models are then compared with the experimental results. It is shown that the numerical results of the 3D particle model agree well with those of the analytical model and the experimental data. And this 3D particle model can also be used for other electric thrusters.


1991 ◽  
Vol 9 (2) ◽  
pp. 312-316 ◽  
Author(s):  
K. K. Foo ◽  
R. P. W. Lawson ◽  
X. Feng ◽  
W. M. Lau
Keyword(s):  
Ion Beam ◽  

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