The invention belongs to a burst rotation speed prediction technology and relates to a trisection grooving prefabrication method for a disc, blade and shaft integrated turbine rotor with ultrahigh rotation speed. The required burst rotation speed can be obtained accurately through groove prefabrication. The method mainly adopts an average stress method for theoretical calculation, and an initial grooving structure is obtained. In combination with a nonlinear finite element analysis method, the trisection burst rotation speed of the disc, blade and shaft integrated turbine rotor with the ultrahigh rotation speed is subjected to numerical simulation analysis, impact factors of a grooving process, a grooving width d, a grooving radius r and a grooving depth h are determined, and the grooving structure is further optimized. A gradual grooving method is adopted during a burst test, the residual sectional area after continuous grooving is a product of the square of the quotient when the burst rotation speed lower limit is divided by the burst rotation speed upper limit and the residual sectional area before grooving, and grooving is performed until the required burst rotation speed is obtained. With adoption of the method, the test times are reduced remarkably, the test efficiency is improved, the test cost is reduced, the method has higher practical application values, and the reliability of a starter system is improved, and the performance of a starter is optimized.