# Analysis of Destructive Effects with Electron Bombardment in Slow-Wave Structures

Authors: Nongchao Tan; Ping Wu; Ye Hua; Jun Sun; Yibing Cao; Guangshuai Zhang; Wenhui Huang; Wenhua Huang
Journal: Laser and Particle Beams
 (2022)

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## Abstract

Radio frequency (RF) breakdown can result in pulse shortening and seriously degrade the stability and reliability of relativistic backward wave oscillators (RBWOs). This paper discusses the energy range of electrons causing breakdown traces in slow-wave structures (SWSs) through particle-in-cell (PIC) simulation, numerical calculation, and experimental verification. The PIC simulation and numerical calculation results reveal that the energy of the majority of the field-induced electrons bombarding the SWS surfaces after being accelerated is less than 120 keV. Furthermore, the micro appearances of the breakdown traces in SWSs and the witness targets bombarded directly by electrons of various energy levels have been analyzed. Scanning electron microscope (SEM) shows that the breakdown traces are featured with corrugated morphologies with a wide range and a shallow depth. A mass of craters emerge in the vicinity of the corrugated morphologies. These appearances are quite similar to destructive traces impacted directly by low-energy electrons (around 160 keV). Thus, it is confirmed that the breakdown traces result from the bombardment of low-energy electrons. Therefore, the breakdown mechanism of field-emitted electrons impacting on the structure surfaces in RBWOs has been further improved.


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## Body

## 1. Introduction

Relativistic backward wave oscillator (RBWO) is one of the most promising high-power microwave (HPM) devices owing to its compact structure, high-conversion efficiency, and repetitive operation [1–8]. In the past several decades, many methods have been proposed to continuously improve the power capacity and pulse width of RBWOs, such as the overmoded structures, the more effective resonant reflector, and the surface treating methods [9–14]. However, with the continuous increase of microwave output power, the intensity of the electromagnetic field on the structure surfaces increases accordingly, which will inevitably lead to the occurrence of radio frequency (RF) breakdown. The existence of RF breakdown causes irreversible structural damage, produces large amount of plasma, results in pulse shortening, and ultimately limits the performance of RBWOs [15–20]. The concept of explosive-electron emission (EEE) has been developed by many researchers to explain the vacuum breakdown in RBWOs [21, 22]. The associated physics includes the Coulomb explosion of microprotrusions at highly localized field-emitting sites, ionization of sputtered material, and the formation of cathode spot plasmas. However, it has been observed experimentally that the breakdown traces are more evident on the opposite sides of the locally strong field spots rather than the sides of the locally strong field, which is difficult to explain by EEE model [23]. Therefore, a few researchers have put forward that field-emitted electrons impacting on structure surfaces may be one of the causes of RF breakdown in RBWOs with a strong external guiding magnetic field [24]. When the strength of the electric field of a local region exceeds the field-emission threshold, field-induced electrons are generated. Afterwards, partial electrons can absorb energy from the RF field. Restricted by a strong guiding magnetic field, the energetic electrons bombard structure surfaces intensively and eventually cause material ablation and plasma formation. In our recent research, by observing the structure surfaces after different high-power microwave pulses, it has been verified experimentally that the breakdown traces on the structure surfaces originate from the bombardment of electrons [24]. However, the energy range of electrons bombarding the structure surfaces needs to be further studied, so as to provide theoretical guidance for proposing corresponding methods to suppress breakdown. In this paper, the formation mechanism of breakdown traces appearing in slow-wave structures (SWSs) after HPM-generation experiment has been analyzed through simulation and experimental verification. By comparing the micro appearances of breakdown traces and witness plates bombarded by electrons of different energy levels, it is concluded that the energy of electrons causing structural damage is mainly less than 160 keV. This paper is organized as follows: in Section 2, field-emitted-electron movement in SWSs is studied using particle-in-cell (PIC) simulation. Section 3 presents single-particle calculation results, in close agreement with the PIC simulation results. Experimental verifications are demonstrated in Section 4. Finally, a brief summary and conclusion are given in Section 5.


## 2. PIC Simulations

Figure1 shows a schematic diagram of an X-band RBWO, which consists of an annular cathode made of graphite, a resonant reflector, seven-period nonuniform SWSs, an extractor, and a beam collector. Under the restriction of an external strengthened magnetic field, an intensive relativistic electron beam (IREB) emitted by the annular cathode successively passes through the reflector, SWSs, and the extractor and ultimately is collected by the beam collector. During the process of IREB transmission, the electrons interact with the first spatial harmonic of the backward wave. The amplified backward wave is reflected by the reflector and becomes a forward wave afterwards. The extractor is mainly used to enhance the beam-microwave power conversion efficiency. Two-dimensional simulation models are carried out using the electromagnetic particle-in-cell (PIC) code UNIPIC, with a 0.25 mm × 0.25 mm uniform grid [25]. With an 890 keV, 12.6 kA electron beam, the output power of the X-band RBWO can reach 5.1 GW. The strongest normal electric field in the SWSs corresponding to the easiest emission of electrons is located in the left-hand side of the fourth high-frequency structure (about 620 kV/cm).Figure 1
Schematic of the X-band RBWO.The electron-emission boundary is set as the small radius of the high-frequency structure ridges, where breakdown traces first appear in the experiment. The beam emission model has been adopted in the PIC simulation. Field-emitted-electron movement in SWSs can be monitored by real and phase spaces. SWS ridges can be divided into two types. The field-emitted electrons produced by several SWS ridges can bombard the opposite sides of the emitting sides after acceleration, as well as the emitting sides. The right-hand side of the first high-frequency structure is given as an example, the real and phase space of the field-emitted electrons at which timet (t = 20 s) is shown in Figure 2. The maximum electric field strength of the right-hand side of the first high-frequency structure is about 500 kV/cm. According to Fowler–Nordheim formula, field-emission current depends on the locally applied electric field, equivalent field-enhancement factor (β), and work function (φw) [26]. In the previous study, β ranges from tens to hundreds [27, 28]. Setting β = 50, φw = 4.3 eV, the corresponding current density is 1.36 × 108 A/m2. Assuming that individual emission microdots are 10 μm in size and 10 emission microdots exist in a single grid, the average current density of the grid can be calculated as 2.17 × 106 A/m2. Furthermore, if the uniform distribution of the electric field along the angular direction is considered, the emission current intensity is 83 A. Through the observation of momentum phase space (Figure 2(b)) and energy phase space (Figure 2(c)), the energy of the electrons that ultimately impacts on the opposite side and bombard back the emitting side is less than 100 keV. Besides, increasing or decreasing the emission current density to some extent has little influence on the emission electron motion. On the other hand, the field-emitted electrons generated by the other ridges of SWS are unable to transit the cavities between SWS rings to bombard the opposite sides; that is, they all return to the emitting sides. The real and phase space of the field-induced electrons at the left-hand side of the fourth high-frequency structure at time t (t = 20 s) is shown in Figure 3. At this time, the maximum electric field strength of the left-hand side of the fourth high-frequency structure is 620 kV/cm. Correspondingly, the average current density of the grid and the emission current intensity are 3.89 × 107 A/m2 and 1.48 kA, respectively. Figure 3(c) shows that the energy of the electrons impacting back the emitting side is in the range of tens of keV.Figure 2
Movement of electrons produced at the right-hand side of the first high-frequency structure at timet (t = 20 s). (a) Real space. (b) Momentum phase space. (c) Energy phase space.
(a)(b)(c)Figure 3
Movement of electrons produced at the left-hand side of the fourth high-frequency structure at timet (t = 20 s). (a) Real space. (b) Momentum phase space. (c) Energy phase space.
(a)(b)(c)


## 3. Numerical Calculations

To further analyze the energy distribution of the field-induced electrons impacting on SWS surfaces, single-particle calculations have been carried out.Similar to the PIC simulation, the initial position of the electrons is set as the small radius of the SWS ridges. Although the field-enhancement factor (β) is taken into consideration, the field-emission current of single microdot obtained using the Fowler–Nordheim formula is only a few amperes, and thus the space-charge field of this current can be negligible [26, 29]. Therefore, the electrons are accelerated under the combined action of the RF electromagnetic field, the space-charge field induced by the IREB, and the external guiding magnetic field. The equation of motion can be written as(1)ddtγmer•−γmerθ•2=−eEr+−erθ•Bz+Bout−z•Bθ,1rdγmer2θ•dt=−ez•Br−r•Bz+Bout+−eEθ,dγmez•dt=−eEz+−er•Bθ−rθ•Br,where Ez, Er, Eθ, Bz, Br, and Bθ comprise the total field, the RF field combined with the space-charge field of the IREB extracted from the PIC simulation results; and Bout suggests the external guiding magnetic field. The amplitude of the total electric field distribution in the SWSs at time t (t = 20 s) is demonstrated in Figure 4. Due to the superposition of the space-charge field of the IREB, the field distribution is distorted in the position of the IREB.Figure 4
The amplitude of the total electric field distribution at timet (t = 20 s).The space gap Δz and time interval Δt of the extracted field are 0.25 mm and T/36, respectively, where Δz denotes the grid size and T the corresponding RF period. The strength of the external magnetic field is selected as 4.3 T. A time-centered differential leaping algorithm is adopted to maintain the propulsion of electron motion as follows:(2)ut+Δt/2−ut−Δt/2Δt=qm0Et+ut+Δt/2+ut−Δt/22γt×Bt.Similar to the PIC simulation (Section2), the results of single-particle calculation can be divided into two categories as well. The movement of field-emitted electrons generated at the right-hand ridge of the first SWS is shown in Figure 5. Due to the superposition of the space-charge field, the emission time of electrons is less than half a microwave period. The field-emitted electrons at the right-hand ridge of the first SWS may be generated from the ninth time step to the nineteenth time step. Besides, only a proportion of the electrons emitted at a specific moment can transit through the cavity and bombard the opposite side, while most of the remaining electrons return to their emitting side. Specifically, most of the electrons generated at the ninth time step can transit through the cavity and bombard the opposite side (Figure 5(a)); in the next time step (the tenth time step), fewer electrons can bombard the opposite side (Figure 5(b)). All the electrons generated in other time steps can only return to their emitting side. The energy distribution of electrons bombarding the opposite side and returning to their own side is illustrated in Figure 6. Different colors represent the electrons generated from the ninth time step to the nineteenth time step. The energy of electrons bombarding both sides is mainly less than 120 keV. For the case where all generated electrons bombard their emitting side, the left-hand ridge of the fourth SWS is discussed as an example. During the emission period, the energy of the electrons that finally bombard back to their emitting side is mainly less than 100 keV, as shown in Figure 7.Figure 5
The axial position of the electrons generated at the ninth time step (a) and the tenth time step (b).
(a)(b)Figure 6
Energy distribution of electrons bombarding the opposite side (a) and the emitting side (b) (different colors indicate the electrons generated from the ninth time step to the nineteenth time step).
(a)(b)Figure 7
Energy distribution of electrons impacting on their emitting side only (different colors represent electrons emitted from the fourth time step to the eighth time step).The PIC simulation and single-particle calculation results reveal that the energy of the field-induced electrons bombarding the structure surfaces after being accelerated is mainly less than 120 keV. To verify this, the morphologies of the witness plates bombarded directly by the electron beam and the breakdown traces of SWSs after the HPM experiment are compared.


## 4. Experimental Results

An experiment involving an electron beam bombarding target plates made of stainless steel (SS) and titanium-alloy has been performed first. The morphologies of the SS witness plates bombarded by different energy electrons were obtained using a scanning electron microscope (SEM) and a three-dimensional confocal laser scanning microscope (CLSM), as shown in Figure8. Compared that high-energy electrons (around 300 keV) are inclined to cause independent pit-like traces with smaller size and deeper depth (Figure 8(c)), the SS’s surface tends to show corrugated morphologies with larger range but shallower depth after low-energy electron bombardment (around 160 keV) (Figure 8(a)). The lower the electron energy, the shallower and wider the damage traces. The three-dimensional morphologies of the damage traces imaged by the CLSM further verify the foregoing conclusion. The maximum depth of the damage traces is 23.5 μm at 163 kV and 48.7 μm at 304 kV (Figures 8(d) and 8(e)). Meanwhile, many craters emerge in the vicinity of corrugated morphologies after being impacted by low-energy electrons (Figure 8(b)). The formation of craters can be explained by the “melting mode” of the interaction between electrons and SS [30]. As electrons strike a material, the maximum energy deposition density is not located on the material’s surface, but at a certain depth inside the material. During the interaction between the electrons and SS, part of the subsurface will reach the melting point first, resulting in the formation of molten droplets. Thereafter, under the quasistatic stress generated by the temperature field gradient, the droplets break through the surface to form eruptions, and near-circular holes are formed.Figure 8
Microscopic images of damage traces on witness plates made of SS using a SEM (a–c) and a CLSM (d, e). (a) Corrugated morphologies appear at a diode voltage of 163 kV and diode current of 1.59 kA. (b) Craters emerge in the vicinity of corrugated morphologies. (c) Independent, pit-like traces at a diode voltage of 304 kV and diode current of 1.58 kA. (d) Three-dimensional morphologies of corrugated morphologies. (e) Three-dimensional morphologies of independent, pit-like traces.After interacting with electron beams, the surface of titanium-alloy witness plates shows destructive traces similar to that of SS, as depicted in Figure9. The maximum depth of damage traces is 40.1 μm at 166 kV and 58.3 μm at 303 kV (Figures 9(c) and 9(d)), deeper than the traces formed on the surface of SS. This phenomenon can be explained by the energy deposition curve of electrons in materials. The density of SS is higher than that of titanium-alloy, so the penetration depth of electrons in SS is shallower, resulting in shallower ablative traces. In addition, unlike SS, no craters can be observed in the vicinity of corrugated morphologies after impacted by low-energy electrons (around 160 keV). The area where the subsurface of titanium-alloy melts is deeper than that of SS; therefore, it is quite difficult for molten droplets to break through the titanium-alloy’s surface and erupt to form craters. If the electron energy is reduced (<160 keV), craters may emerge after interaction with electrons.Figure 9
Microscopy images of damage traces on the titanium-alloy’s witness plates using a SEM (a, b) and a CLSM (c, d). (a) Corrugated morphologies appear at a diode voltage of 166 kV and diode current of 1.58 kA. (b) Independent, pit-like traces at a diode voltage of 303 kV and diode current of 1.60 kA. (c) Three-dimensional morphologies of corrugated morphologies. (d) Three-dimensional morphologies of independent, pit-like traces.
(a)(b)(c)(d)Subsequently, a HPM-generation experiment on the X-band RBWO is performed on TPG-1000 high-current electron beam accelerator. Breakdown traces are evident on the SWSs’ working surfaces after the experiment, as shown in Figure10. The breakdown traces on both sides of several SWSs show distinct symmetry after about 100 pulses (Figure 10(a)), which is in accordance with the PIC simulation and single-particle calculation, the field-induced electrons generated by some SWS ridges bombard the opposite sides and simultaneously impact on their emitting sides. As the number of pulses increases, the symmetry of breakdown traces tends to be blurred (Figure 10(b)).Figure 10
Evident breakdown traces in SWSs after the HPM-generation experiment: (a) after about 100 pulses. (b) After about 2000 pulses.
(a)(b)Images of the breakdown traces on the working surface of left wall of the fourth SWS are obtained using a SEM and are shown in Figure11 (SS’s surface) and Figure 12 (titanium-alloy’s surface). The surface of SS shows regularly spaced lines which are generated by mechanical polishing before HPM experiment (Figure 11(a)). The breakdown traces on the SS’s surface entirely exhibit corrugated morphologies rather than deep pit-like traces (Figure 11(b)), and many craters emerge in the vicinity of corrugated morphologies (Figure 11(c)). These appearances are quite similar to those concerning traces left by low-energy electron bombardment. In addition, the breakdown traces on the titanium-alloy’s surface exhibit shallower, wrinkle-shaped morphologies when compared to the traces from low-energy electron bombardment (around 160 keV). Simultaneously, a large number of craters are observed in the vicinity of wrinkle-shaped morphologies (Figure 12(c)), while no craters can be observed after direct low-energy electron bombardment. These findings indicate the energy of the majority of electrons that impact on SWS surfaces, therefore, is less than 160 keV; this is in good agreement with the PIC simulation and single-particle calculation.Figure 11
Typical micromorphologies of the SS SWSs: (a) before HPM experiment. (b) Corrugated morphology. (c) Craters.
(a)(b)(c)Figure 12
Typical micromorphologies of the titanium-alloy SWSs: (a) before HPM experiment. (b) Corrugated morphology. (c) Craters.
(a)(b)(c)


## 5. Conclusion

This paper presents PIC simulation, single-particle calculation, and experimental research to explore the energy range of electrons bombarding the SWS’s surfaces in an X-band RBWO. The investigation reveals that the field-induced electrons can bombard the opposite side or impact back on the emitting side, the energy of which is mainly less than 120 keV. Through the comparison of the micro appearances of the witness targets bombarded directly by electrons with various energy levels and the breakdown traces in SWSs, it is determined that the energy of electrons bombarding the surface of the structures is mainly below 160 keV, which is in accordance with the PIC simulation and numerical calculation results. In future work, we intend to explore possible suppression methods to restrain breakdown in RBWOs.



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