In the previous studies, an instrumented Taylor impact test was established to measure the stress-strain curve at an ultrahigh strain rate. To calculate the axial stress distribution in the specimen, a bi-linearity of the internal force distribution in both the elasticity- and plasticity-dominant regions was assumed. However, the unavoidably generated excessive local deformation (ELD) near the impact surface results in early unloading and a strong nonlinear distribution of the internal force in the region near the impact surface. Consequently, the measurable stress-strain curve was limited to 0.1 of the axial strain. On the other hand, the pulse-shaping technique, which is widely used in split Hopkinson pressure bar tests, can be employed to increase the strain until the stress-strain curve is measurable through Taylor impact tests because the short rise time is considered to be a possible reason of ELD generation. For the first time, this study introduced the pulse-shaping technique to the instrumented Taylor impact test to expand the measurability of the stress-strain curve to a higher strain range. To suppress the ELD, the dimensions of the pulse shaper are determined through finite element analyses after a discussion of the mechanism to suppress ELD. Then, the proposed method with a newly designed specimen is validated conducting the real Taylor impact test.