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Efficiency, performance limits and scaling of rail launchers

机译:轨道发射器的效率,性能限制和扩展

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The fundamental parameters that influence the performance and efficiency of rail launchers are shown to be: mechanical energy/bore volume (p/sub 0/), effective magnetic flux density (B/sub 0/) and the total mass/effective bore area (m). To achieve a high electrical efficiency these parameters should be minimized by increasing the bore diameter and reducing the bore length, subject to other design constraints such as increasing launch package mass. The efficiency of rail launchers is limited by energy losses in the rail and armature, arcing losses following transition and the barrel residual magnetic energy at exit. These are derived analytically including the effect of field diffusion, velocity skin-effect (VSE), predicted transition velocities and arcing phenomena. A range of aluminium alloy armatures with breech-fed copper rails are considered with kinetic energies up to 20 MJ and bore diameters from 40 to 180 mm. Electrical efficiencies for 10 and 20 MJ kinetic energy launchers with minimum diameters are estimated to be 52 and 62% respectively. An increase in efficiency to 67% is predicted for larger diameter launchers with transition velocities increased to <2.0 km/s due to lower energy density and electrical action.
机译:影响轨道发射器性能和效率的基本参数显示为:机械能/孔体积(p / sub 0 /),有效磁通密度(B / sub 0 /)和总质量/有效孔面积( m)。为了获得较高的电效率,应根据其他设计约束(例如增加发射组件的质量),通过增加孔径和减小孔径来最小化这些参数。轨道发射器的效率受到轨道和电枢中的能量损耗,过渡后的电弧损耗以及出口处的枪管残余磁能的限制。这些是通过分析得出的,包括场扩散,速度趋肤效应(VSE),预测的转变速度和电弧现象的影响。一系列带有后膛馈送铜轨的铝合金电枢被认为具有高达20 MJ的动能和40至180 mm的内径。最小直径的10和20 MJ动能发射器的电效率分别估计为52%和62%。对于较大直径的发射器,由于较低的能量密度和电作用,其转换速度增加至<2.0 km / s,预计效率将提高到67%。

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