2. Collisions in a weakly magnetized plasma

To consider the effect of a finite electron gyroradius on effective collisions below we use the full expression of the Landau form of the collision integral $Y[f]=-m^{-1}(\boldsymbol{{\rm\nabla}}\boldsymbol{\cdot }\boldsymbol{s})$ where the density of particle flux $\boldsymbol{s}$ has the following components (Pitaevskii & Lifshitz Reference Pitaevskii and Lifshitz1981):

(2.1) $$\begin{eqnarray}\displaystyle s_{{\it\alpha}} & = & \displaystyle \frac{{\rm\pi}e^{2}{\it\Lambda}}{m}\mathop{\sum }_{{\it\beta}}\int \left(\frac{\partial f(\boldsymbol{v}^{\prime })}{\partial v_{{\it\beta}}^{\prime }}+\frac{mv_{{\it\beta}}^{\prime }}{T}f(\boldsymbol{v}^{\prime })\right)f_{0}(\boldsymbol{v})\frac{w^{2}{\it\delta}_{{\it\beta}{\it\alpha}}-w_{{\it\alpha}}w_{{\it\beta}}}{w^{2}}\,\text{d}\boldsymbol{v}^{\prime }\nonumber\\ \displaystyle & & \displaystyle -\,\frac{{\rm\pi}e^{2}{\it\Lambda}}{m}\mathop{\sum }_{{\it\beta}}\int \left(\frac{\partial f(\boldsymbol{v})}{\partial v_{{\it\beta}}}+\frac{mv_{{\it\beta}}}{T}f(\boldsymbol{v})\right)f_{0}(\boldsymbol{v}^{\prime })\frac{w^{2}{\it\delta}_{{\it\beta}{\it\alpha}}-w_{{\it\alpha}}w_{{\it\beta}}}{w^{2}}\,\text{d}\boldsymbol{v}^{\prime },\end{eqnarray}$$

where $\boldsymbol{w}=\boldsymbol{v}-\boldsymbol{v}^{\prime }$ , ${\it\alpha},{\it\beta}=x,y,z$ , ${\it\Lambda}=\ln ({\it\lambda}_{D}q^{2}/T)$ and ${\it\lambda}_{D}$ is the Debye length.

Considering the perturbation ${\it\delta}f=f(\boldsymbol{v})\exp (\text{i}{\it\Phi})$ of the initial distribution function $f_{0}(\boldsymbol{v})$ , the phase of the perturbation is ${\it\Phi}=\boldsymbol{k}\boldsymbol{\cdot }\boldsymbol{r}-{\it\omega}t$ . The corresponding perturbations to the electromagnetic field are ${\it\delta}\boldsymbol{B}=\boldsymbol{B}\exp (\text{i}{\it\Phi})$ , ${\it\delta}\boldsymbol{E}=\boldsymbol{E}\exp (\text{i}{\it\Phi})$ , while the background magnetic field is $\boldsymbol{B}_{0}=B_{0}\boldsymbol{e}_{z}$ . The wave vector of perturbations $\boldsymbol{k}$ is assumed to lie in the $(x,z)$ plane. In this case, the perturbation of the Valsov equation takes the form

(2.2) $$\begin{eqnarray}\frac{\partial {\it\delta}f}{\partial t}+\boldsymbol{v}\frac{\partial {\it\delta}f}{\partial \boldsymbol{r}}+\frac{q}{mc}[\boldsymbol{v}\times \boldsymbol{B}_{0}]\frac{\partial {\it\delta}f}{\partial \boldsymbol{v}}+Y[{\it\delta}f]=-\frac{q}{m}\left({\it\delta}\boldsymbol{E}+\frac{1}{c}[\boldsymbol{v}\times {\it\delta}\boldsymbol{B}]\right)\frac{\partial f_{0}}{\partial \boldsymbol{v}}.\end{eqnarray}$$

We introduce the force $\boldsymbol{F}=(q/m)(\boldsymbol{E}+c^{-1}[\boldsymbol{v}\times \boldsymbol{B}])$ , cylindrical velocity coordinates $v_{x}=v_{\bot }\cos {\it\theta}$ , $v_{y}=v_{\bot }\sin {\it\theta}$ and rewrite (2.2) as

(2.3) $$\begin{eqnarray}-\text{i}{\it\omega}{\it\delta}f+\text{i}k_{z}v_{z}{\it\delta}f+\text{i}k_{x}v_{\bot }\cos {\it\theta}{\it\delta}f-\frac{qB_{0}}{mc}\frac{\partial {\it\delta}f}{\partial {\it\theta}}+Y[{\it\delta}f]=-\frac{q}{m}\boldsymbol{F}\text{e}^{\text{i}{\it\Phi}}\frac{\partial f_{0}}{\partial \boldsymbol{v}},\end{eqnarray}$$

where $[\boldsymbol{v}\times \boldsymbol{B}_{0}](\partial /\partial \boldsymbol{v})=-B_{0}(\partial /\partial {\it\theta})$ . Then we divide (2.3) by $\exp (\text{i}{\it\Phi})$ and introduce ${\it\Omega}_{0}=qB_{0}/mc$ , ${\it\lambda}={\it\omega}-k_{z}v_{z}$ :

(2.4) $$\begin{eqnarray}-\text{i}({\it\lambda}-k_{x}v_{\bot }\cos {\it\theta})f-{\it\Omega}_{0}\frac{\partial f}{\partial {\it\theta}}+Y[f]=-\boldsymbol{F}\frac{\partial f_{0}}{\partial \boldsymbol{v}}.\end{eqnarray}$$

We introduce the function $W=({\it\lambda}{\it\theta}-k_{x}v_{\bot }\cos {\it\theta})/{\it\Omega}_{0}$ and function $g(\boldsymbol{v})=f(\boldsymbol{v})\exp (\text{i}W)$ . Thus, (2.4) can be rewritten as

(2.5) $$\begin{eqnarray}\frac{\partial g}{\partial {\it\theta}}+\text{e}^{\text{i}W}Y[g\text{e}^{-\text{i}W}]=-\boldsymbol{F}\frac{\partial f_{0}}{\partial \boldsymbol{v}}\text{e}^{\text{i}W}.\end{eqnarray}$$

To derive the dispersion relation for perturbations, one should substitute into (2.5) the Maxwell equations for electromagnetic field perturbations ( ${\sim}\boldsymbol{F}$ ) expressed through function $g$ (see, e.g. Zelenyi & Artemyev Reference Zelenyi and Artemyev2013). In this case, the final wave frequency/growth rate would depend on collision frequency (e.g. for the simplified collision integral (1.1) the operator $Y$ is proportional to collision frequency  ${\it\nu}$ ). However, we would like to estimate the effect of a finite electron gyroradius on collision frequency ${\it\nu}$ . Thus, we compare the term ${\sim}Y$ for the two systems: when simplified (1.1) can be used and $Y\sim {\it\nu}$ and when the full collision integral $Y[f]=-m^{-1}(\boldsymbol{{\rm\nabla}}\boldsymbol{\cdot }\boldsymbol{s})$ with (2.1) should be taken into account. For this reason, we carefully consider the second term in (2.5) and estimate the main part of this term

(2.6) $$\begin{eqnarray}\int ^{{\it\theta}}\text{e}^{\text{i}W}Y[g\text{e}^{-\text{i}W}]\,\text{d}{\it\theta}.\end{eqnarray}$$

In the limit $k_{x}\sqrt{2T/m}/{\it\Omega}_{0}\gg 1$ , function $g\exp (-\text{i}W)$ contains the fast oscillating term ${\sim}\exp (\text{i}k_{x}v_{\bot }\sin {\it\theta}/{\it\Omega}_{0})=\exp (\text{i}k_{x}v_{y}/{\it\Omega}_{0})$ . Thus, in (2.1) we should keep the main terms corresponding to the derivative $\partial f/\partial v_{y}$ . The first term in (2.1) contains the integral $\int (\partial f/\partial v_{y}^{\prime })\,\text{d}v_{y}^{\prime }\sim f$ . Therefore, the second term with $\partial f/\partial v_{y}$ is more important and we can write:

(2.7) $$\begin{eqnarray}\displaystyle & \displaystyle s_{{\it\alpha}}\approx -\frac{{\rm\pi}e^{2}{\it\Lambda}}{m}\left(\frac{\partial f(\boldsymbol{v})}{\partial v_{y}}+\frac{mv_{y}}{T}f(\boldsymbol{v})\right)A_{{\it\alpha}}(\boldsymbol{v}) & \displaystyle\end{eqnarray}$$

(2.8) $$\begin{eqnarray}\displaystyle & \displaystyle A_{{\it\alpha}}(\boldsymbol{v})=\int f_{0}(\boldsymbol{v}^{\prime })\frac{w^{2}{\it\delta}_{y{\it\alpha}}-w_{y}w_{{\it\beta}}}{w^{2}}\,\text{d}\boldsymbol{v}^{\prime }. & \displaystyle\end{eqnarray}$$

The main part of $s_{{\it\alpha}}$ from (2.8) is

(2.9) $$\begin{eqnarray}s_{{\it\alpha}}\approx -\text{i}\frac{k_{x}}{{\it\Omega}_{0}}\frac{{\rm\pi}e^{2}{\it\Lambda}}{m}g(\boldsymbol{v})\text{e}^{-\text{i}W}A_{{\it\alpha}}(\boldsymbol{v}).\end{eqnarray}$$

Thus, the integrand of (2.6) takes the form

(2.10) $$\begin{eqnarray}\text{e}^{\text{i}W}Y[g\text{e}^{-\text{i}W}]=-\frac{k_{x}^{2}}{{\it\Omega}_{0}^{2}}\frac{{\rm\pi}e^{2}{\it\Lambda}}{m^{2}}g(\boldsymbol{v})A_{{\it\alpha}}(\boldsymbol{v}).\end{eqnarray}$$

In dimensionless form (2.10) can be written as

(2.11) $$\begin{eqnarray}\text{e}^{\text{i}W}Y[g\text{e}^{-\text{i}W}]=-\frac{2k_{x}^{2}T}{{\it\Omega}_{0}^{2}m}{\tilde{Y}}[f]\text{e}^{\text{i}W},\end{eqnarray}$$

where ${\tilde{Y}}$ is the initial collision integral (2.1) without derivatives over fast oscillation terms. Equation (2.11) shows that the effect of a finite electron gyroradius provides the multiplication factor $2k_{x}^{2}T/{\it\Omega}_{0}^{2}m$ . This factor is omitted in the simplified form of the collision integral (1.1). Therefore, if we operate with the collision frequency ${\it\nu}$ from (1.1) then this expression for collision frequency ${\it\nu}$ (Coulomb or effective) should be multiplied by the term $2k_{x}^{2}T/{\it\Omega}_{0}^{2}m\gg 1$ . Of course, for a complete investigation of system stability one should consider the full collision integral (2.1), but for many applications the simplified approach with collision frequency ${\it\nu}$ can be applied with the corresponding correction ${\sim}2k_{x}^{2}T/{\it\Omega}_{0}^{2}m$ . Finally, we come to the following expression for the effective collision frequency in a system with weakly magnetized electrons:

(2.12) $$\begin{eqnarray}{\it\nu}_{eff}\approx \left\{\begin{array}{@{}ll@{}}{\it\nu}(k_{x}{\it\rho}_{e})^{2}\quad & k_{x}{\it\rho}_{e}>1\\ {\it\nu}\quad & k_{x}{\it\rho}_{e}\leqslant 1,\end{array}\right.\end{eqnarray}$$

where ${\it\rho}_{e}=\sqrt{2T/m}/{\it\Omega}_{0}$ is the electron gyroradius. Note, that (2.12) provides only a simplified estimate of the effect of electron finite gyroradius on system stability. However, this simplified expression gives us the opportunity to estimate this effect for realistic system parameters. In the next section we use the modified collision frequency (2.12) to estimate the effect of effective conductivity in the regions with weak magnetic field, in particular in the reconnection regions in near-Earth plasma systems.

3. Estimates of $k_{x}{\it\rho}_{e}$ parameter for space plasma reconnection systems

Let us consider the classical 2-D X-line with magnetic field configuration $\boldsymbol{B}=B_{0}(z/L_{z})\boldsymbol{e}_{x}+B_{z}(x/L_{x})\boldsymbol{e}_{z}$ (see scheme in figure 1). The reversal of the $B_{x}$ magnetic field component in the neutral plane $z=0$ generates so-called neutral region $|z|<\sqrt{{\it\rho}_{0}L_{z}}$ with ${\it\rho}_{0}=\sqrt{2Tm}c/eB_{0}$ where particles are not affected by the $B_{x}$ magnetic field and can move practically freely along the $y$ -axis (Dobrowolny Reference Dobrowolny1968). The same region appears around the $x=0$ plane due to $B_{z}$ reversal: $|x|<\sqrt{{\it\rho}_{z}L_{x}}$ with ${\it\rho}_{z}=\sqrt{2Tm}c/eB_{z}$ . Particles, moving within this region are affected by the effective (averaged gyroradius) magnetic field with amplitude $\tilde{B}_{z}=B_{z}\sqrt{{\it\rho}_{z}L_{x}}/L_{x}=B_{z}\sqrt{{\it\rho}_{z}/L_{x}}$ , while the effective particle gyroradius is equal to the spatial scale ${\it\rho}_{e}=\sqrt{2Tm}c/e\tilde{B}_{z}=\sqrt{{\it\rho}_{z}L_{x}}$ . If we assume that the X-line is generated by the tearing instability with a wavelength equal to $L_{x}=2{\rm\pi}/k_{x}$ (see the scheme in figure 1), then the factor from (2.12) can be written as

(3.1) $$\begin{eqnarray}X=(k_{x}{\it\rho}_{e})^{2}={\it\rho}_{z}L_{x}\left(\frac{2{\rm\pi}}{L_{x}}\right)^{2}=4{\rm\pi}^{2}\frac{{\it\rho}_{z}}{L_{x}}.\end{eqnarray}$$

Figure 2 shows values of $X$ as a function of electron temperature $T$ , $L_{x}$ and $B_{z}$ . For the initial stage of the tearing instability (when $B_{z}$ is still very small) with a wavelength $L_{x}$ which is not too long the factor $X$ is larger than one. Thus, the effect of a finite electron gyroradius can amplify energy dissipation due to effective collisions.

Figure 1.

Schematic view of the X-line region.

Figure 2.

Factor $X$ as a function of $L_{x}$ for two values of $B_{z}$ and four values of electron temperature $T$ .

To estimate the effect of the factor $X$ on magnetic reconnection in real plasma systems we consider the effective collisions induced by two types of turbulence: lower-hybrid drift (LHD) turbulence (Huba et al. Reference Huba, Gladd and Papadopoulos1977) and kinetic Alfvén wave (KAW) turbulence (Chaston et al. Reference Chaston, Johnson, Wilber, Acuna, Goldstein and Reme2009).

Wavelengths of the electromagnetic LHD mode ( ${\sim}{\it\rho}_{e}\sqrt{m_{i}/m_{e}}$ (Daughton Reference Daughton2003)) and KAW ( ${<}0.3{\it\rho}_{e}(m_{i}/me)$ (Voitenko Reference Voitenko1998; Chen et al. Reference Chen, Wu, Zhao, Tang and Huang2014)) are small enough to consider these waves to be small-scale magnetic field perturbations for the large-scale reconnection process. On the other hand, these modes effectively interact both with ions (through the Cherenkov resonance $\boldsymbol{k}\boldsymbol{v}={\it\omega}$ (Karney Reference Karney1978; Karimabadi et al. Reference Karimabadi, Akimoto, Omidi and Menyuk1990; Chaston et al. Reference Chaston, Bonnell, Wygant, Mozer, Bale, Kersten, Breneman, Kletzing, Kurth and Hospodarsky2014)) and electrons (through the Landau resonance $k_{\Vert }v_{\Vert }={\it\omega}$ (Hasegawa Reference Hasegawa1976; Cairns & McMillan Reference Cairns and McMillan2005)). Both modes are widely observed in the vicinity of the reconnection region where their contributions to the electromagnetic field turbulence are the strongest among wave modes (Eastwood et al. Reference Eastwood, Phan, Bale and Tjulin2009; Fujimoto, Shinohara & Kojima Reference Fujimoto, Shinohara and Kojima2011; Huang et al. Reference Huang, Zhou, Sahraoui, Vaivads, Deng, André, He, Fu, Li and Yuan2012). Thus, LHD and KAW can the provide an exchange of energy between the ions and electrons, supporting the anomalous (effective) conductivity. The general form of the frequency of effective collisions ${\it\nu}$ is provided by the quasi-linear equation (Galeev & Sagdeev Reference Galeev, Sagdeev and Leontovich1979):

(3.2) $$\begin{eqnarray}{\it\nu}=\frac{1}{mn_{0}v_{D}}\int W_{k}\frac{{\it\Gamma}(k)}{{\it\omega}(k)}k\frac{\text{d}^{3}k}{(2{\rm\pi})^{3}},\end{eqnarray}$$

where $v_{D}$ is particle drift velocity (i.e. $en_{0}v_{D}$ is a current density), ${\it\Gamma}(k)$ is a wave growth/damping rate, ${\it\omega}(k)$ is a wave frequency and $W_{k}$ is a wave energy density. For current sheet configurations the maximum value of ${\it\nu}_{LHD}$ was derived by Huba, Drake & Gladd (Reference Huba, Drake and Gladd1980):

(3.3) $$\begin{eqnarray}{\it\nu}_{LHD}\approx \frac{{\it\omega}_{pe}^{2}}{{\it\omega}_{LH}}\frac{E_{y}^{2}}{8{\rm\pi}n_{0}T_{e}},\end{eqnarray}$$

where ${\it\omega}_{pe}$ is the plasma frequency, ${\it\omega}_{LH}\approx {\it\Omega}_{e}\sqrt{m_{e}/m_{i}}$ and ${\it\Omega}_{e}=eB_{z}/m_{e}c$ is the electron gyrofrequency, $T_{e}$ is electron temperature and $E_{y}$ corresponds to the amplitude of wave electric field oscillations.

For KAW the maximum growth rate corresponds to Landau excitation ${\it\Gamma}\approx {\it\omega}/kv_{D}$ (Hasegawa & Mima Reference Hasegawa and Mima1978) where the wave frequency is ${\it\omega}_{KAW}=k_{\Vert }v_{A}\sqrt{1+(k_{\bot }{\it\rho}_{i})^{2}}$ with ion gyroradius ${\it\rho}_{i}$ and Alfvén velocity $v_{A}$ (Hasegawa Reference Hasegawa1976). The corresponding collision frequency can be estimated as

(3.4) $$\begin{eqnarray}{\it\nu}_{KAW}\approx {\it\omega}_{KAW}{\it\Gamma}\frac{{\it\omega}_{pe}^{2}}{k_{\Vert }^{2}v_{Te}^{2}}\frac{E_{y}^{2}}{4{\rm\pi}n_{0}m_{e}v_{D}^{2}}\approx \frac{{\it\omega}_{pe}^{2}}{{\it\omega}_{KAW}}\frac{v_{A}^{3}}{v_{D}^{2}v_{Ti}}\frac{E_{y}^{2}}{8{\rm\pi}n_{0}T_{e}}\approx \frac{{\it\omega}_{pe}^{2}}{{\it\omega}_{KAW}}\frac{E_{y}^{2}}{8{\rm\pi}n_{0}T_{e}},\end{eqnarray}$$

where we take into account that $k_{\bot }{\it\rho}_{i}\sim 1$ , $v_{D}\sim v_{Ti}\sim v_{A}$ .

Following Coroniti (Reference Coroniti1985), one can determine the critical amplitude of electric field energy $E_{y}^{2}$ necessary to organize the magnetic field dissipation within the domain with spatial scale ${\sim}L_{z}\sim {\it\rho}_{i}$ :

(3.5) $$\begin{eqnarray}\displaystyle & \displaystyle \frac{(E_{y}^{2})_{LHD}}{8{\rm\pi}n_{0}T_{e}}=\frac{M_{A}}{X}\sqrt{\frac{m_{i}}{m_{e}}}\frac{v_{A}v_{Ti}}{c^{2}}\approx \frac{M_{A}}{X}\sqrt{\frac{m_{i}}{m_{e}}}\left(\frac{v_{A}}{c}\right)^{2} & \displaystyle\end{eqnarray}$$

(3.6) $$\begin{eqnarray}\displaystyle & \displaystyle \frac{(E_{y}^{2})_{KAW}}{8{\rm\pi}n_{0}T_{e}}=\frac{M_{A}}{X}\frac{{\it\omega}_{KAW}}{{\it\Omega}_{i}}\left(\frac{v_{A}}{c}\right)^{2}\approx \frac{M_{A}}{X}\left(\frac{v_{A}}{c}\right)^{2}, & \displaystyle\end{eqnarray}$$

where $M_{A}$ is an Alfvén–Mach number for a particle flowing to the reconnection region. Generally $M_{A}\sim 0.1$ for magnetospheric physics, while $(v_{A}/c)^{2}\approx 10^{-5}$ for the Earth’s magnetotail. Equation (3.6) shows that one can decrease the estimate for the critical amplitude of wave electric field proportionally to ${\sim}1/\sqrt{X}\sim 1/3{-}1/10$ (see figure 2) after taking into account the Pitaevskii effect. For magnetotail current sheets the typical amplitude of LHD waves can reach $10~\text{mV}~\text{m}^{-1}$ (Eastwood et al. Reference Eastwood, Phan, Bale and Tjulin2009; Fujimoto et al. Reference Fujimoto, Shinohara and Kojima2011; Norgren et al. Reference Norgren, Vaivads, Khotyaintsev and André2012), while the estimate of the amplitude from (3.6) is $\sqrt{(E_{y}^{2})_{LHD}}\sim 30/\sqrt{X}~\text{mV}~\text{m}^{-1}$ (Coroniti Reference Coroniti1985). Thus, a factor $X\sim 10$ can help to produce the necessary magnetic energy dissipation due to effective collisions. Amplitudes of KAW electric field are often weaker ${\sim}1~\text{mV}~\text{m}^{-1}$ (Chaston et al. Reference Chaston, Bonnell, Clausen and Angelopoulos2012). The critical amplitude for KAW is $\sqrt{(E_{y}^{2})_{KAW}}$ is of the order of ${\sim}1/\sqrt{X}~\text{mV}~\text{m}^{-1}$ . The Pitaevskii effect of reducing the estimate (3.6) 2–3 times demonstrates an important role of KAW in running magnetic reconnection. Therefore, we conclude that in realistic magnetotail conditions for both cases (LHDI and KAW) the effect of finite electron gyroradius can increase effective collisions and help to overturn Coroniti (Reference Coroniti1985) objections.

4. Discussion and conclusions

The additional effect of the enhancement of effective collisions for $k{\it\rho}_{e}>1$ perturbations was taken into account in the analysis of the electron resistive tearing mode (Zelenyi & Taktakishvili Reference Zelenyi and Taktakishvili1981). This mode is excited by ${\it\nu}\neq 0$ with the growth rate ${\it\gamma}={\it\nu}\text{X}({\it\gamma}_{0}/k_{x}\sqrt{2T_{e}m_{e}})$ where ${\it\gamma}_{0}/k_{x}\sqrt{2T_{e}m_{e}}=2{\rm\pi}^{-1/2}({\it\rho}_{e}/L_{z})^{3/2}(1-k_{x}^{2}L_{z}^{2})/k_{x}L_{z}$ is the growth rate of the electron tearing mode (Laval et al. Reference Laval, Pellat and Vuillemin1966; Galeev & Sudan Reference Galeev and Sudan1985). Therefore, for $X$ factor high enough, the growth rate of the resistive tearing mode increases. This mode is produced by effective collisions and cannot be stabilized by electron magnetization (in contrast to the classical electron tearing mode (Schindler Reference Schindler1974; Galeev & Zelenyi Reference Galeev and Zelenyi1976)). Moreover, for a tearing mode with $k{\it\rho}_{e}>1$ the WKB approximation in the investigation of current sheet stability can be safely applied (Lembege & Pellat Reference Lembege and Pellat1982) supporting the validity of the expressions for the growth rates ${\it\gamma}$ and ${\it\gamma}_{0}$ derived for the case where the wavelength is not too long.

Effective collisions are often considered in numerical models of magnetic reconnection as a trigger for the reconnection process (Daughton, Lapenta & Ricci Reference Daughton, Lapenta and Ricci2004; Daughton et al. Reference Daughton, Roytershteyn, Karimabadi, Yin, Albright, Bergen and Bowers2011; Karimabadi et al. Reference Karimabadi, Roytershteyn, Daughton and Liu2013). In this case, estimates of the reconnection rate can be based on the classical theory of an effective conductivity (Galeev & Sudan Reference Galeev and Sudan1985; Yoon & Lui Reference Yoon and Lui2006) with a proper estimate for the effective collision rate. Thus, the effect of fine structured velocity distributions (when ${\it\rho}k_{x}>1$ ) can be very important. The same effect can be provided by numerical resistivity which supports the slow growth of magnetic islands when the tearing instability is saturated by nonlinear effects (Lipatov & Zelenyi Reference Lipatov and Zelenyi1982).

Figure 2 shows that the most pronounced effect of a finite electron gyroradius corresponds to small-scale reconnection (i.e. small $L_{x}$ ) where instead of one large-scale X-line we deal with a chain of small-scale magnetic islands. Indeed, strong anisotropy of electrons accelerated in the primary reconnection region generates high-amplitude curvature currents (Egedal, Le & Daughton Reference Egedal, Le and Daughton2013; Artemyev et al. Reference Artemyev, Petrukovich, Nakamura and Zelenyi2015) responsible for the formation of very thin current sheets with vanishing $B_{z}$ magnetic field (Nakamura et al. Reference Nakamura, Baumjohann, Runov and Asano2006; Artemyev et al. Reference Artemyev, Petrukovich, Frank, Nakamura and Zelenyi2013; Le et al. Reference Le, Egedal, Ng, Karimabadi, Scudder, Roytershteyn, Daughton and Liu2014). Instability of such thin current sheets results in secondary reconnection in the outflow region of the primary large-scale X-line (so-called plasmoid instability) with the corresponding birth of a multitude of small-scale X- and O-magnetic points (Daughton et al. Reference Daughton, Roytershteyn, Karimabadi, Yin, Albright, Bergen and Bowers2011; Huang, Bhattacharjee & Forbes Reference Huang, Bhattacharjee and Forbes2013). Thus, the secondary reconnection of such thin current sheets can occur within the region of $k_{x}{\it\rho}_{e}>1$ . To illustrate this scenario we show two events of Cluster spacecraft observations of magnetic reconnection in the Earth’s magnetotail (see figure 3). The characteristic $B_{z}$ reversal and plasma flows $v_{x}$ indicate that Cluster is in close vicinity to the X-line. We calculate the electron gyroradius ${\it\rho}_{e}$ using local measurements of the $B_{z}$ and $B_{y}$ magnetic field ( $B_{x}$ is assumed to be zero). Around the X-line ${\it\rho}_{e}$ reaches ${\sim}1000~\text{km}$ , thus $X$ becomes larger than one for $L_{x}<6R_{E}$ . For example, the secondary reconnection with a wavelength of approximately ${\sim}2R_{E}$ corresponds to an increase of effective collision frequency by a factor $X\sim 3$ . We also note that for both events shown in figure 3, current sheet thicknesses were approximately ${\sim}800~\text{km}$ and ${\sim}600~\text{km}$ (see estimates of current density amplitudes in Artemyev et al. Reference Artemyev, Petrukovich, Nakamura and Zelenyi2015). Thus, for $L_{x}\sim 2R_{E}$ the ratio $L_{x}/L_{z}\sim 18$ and the corresponding current sheets are very prolonged and stretched.

Figure 3.

Two cases of Cluster spacecraft crossing a reconnection region (see the characteristic reversal of $B_{z}$ ). Both cases are taken from Artemyev et al. (Reference Artemyev, Petrukovich, Nakamura and Zelenyi2015).

To conclude, we consider the effects of a finite electron gyroradius for current sheet stability in the case when effective collisions are present in the system. Following Pitaevskii (Reference Pitaevskii1963) we demonstrate that a fast electron gyrorotation results in a fine structure of the perturbations of the electron distribution function. As a result, the full expression for the collision integral gives a multiplication factor $\text{X}\sim (k_{x}{\it\rho}_{e})^{2}$ for collision frequency (where $k_{x}$ is a transverse wavenumber). For realistic conditions in the Earth’s magnetotail this factor can often be larger than one and thus can increase the effect of particle scattering by electromagnetic turbulence. We show that effect of a finite electron gyroradius should be particularly strong for the secondary reconnection of very thin current sheets formed in the outflow region of the primary X-line.