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已经证明带尾翼爆炸成形侵彻体（ＥＦＰ）技术的推广提供了许多好处，例如控制ＥＦＰ尾部的皱褶，因此增加杆的密实性和性能，以及改善气动力特性。因为已经证明了将形成尾翼的许多方法实现或者集成在一个给定的战斗部结构上是有某些困难的。因此介绍一个在ＥＦＰ上形成尾翼的改进方法，它使用简单的制造方法使之容易集成。该工艺包括粘接一个适当形状的薄金属片到药形罩的凸侧，并且几乎不需要改变战斗部的壳体和药形罩。使用这个形成尾翼的金属片方法，可能导致一个期望的旋转运动。此外，使用这种形成尾翼的方法，能够不改变炸药或者作用波形控制器或者使用昂贵的多点起爆系统。通过使用战斗部壳体周期性的不对称调整尾翼形成机理，能够产生旋转运动。与分析结果和试验结果同时讨论尾翼形成方法的细节，给出形成工艺的进一步分析。此外，讨论气动力特性证明尾翼ＥＦＰ和最佳旋转的好处。最后，给出终点性能数据。
The rollout of EOF technology has proven to offer many benefits such as controlling wrinkles in the tail of the EFP, thereby increasing rod density and performance, and improving aerodynamic properties. Since it has proven somewhat difficult to implement or integrate many methods of forming the tail into a given warhead structure. Therefore, an improved method of forming a tail on the EFP is introduced, which is easy to integrate using a simple manufacturing method. The process involves bonding a thin sheet of a suitable shape to the convex side of the lance and requiring little or no change to the shell and lance of the lance. Using this finned sheet metal method can result in a desired rotational movement. In addition, with this method of forming the empennage, explosives or active waveform controllers can be changed or expensive multi-point detonation systems can be used. The rotational movement can be produced by periodically and asymmetrically adjusting the empennage forming mechanism using the shell of the warhead. The details of the empennage formation method are discussed along with the analysis and test results, giving further analysis of the formation process. In addition, discuss the aerodynamic characteristics that demonstrate the benefits of the EFP tail and optimal rotation. Finally, the end point performance data is given.