CFD; Computational Fluid Dynamics; Rocket Nose Cone; Rocket Science; Mach Number; Subsonic; Transonic; Supersonic; Space Launch; SLV; Satellite Launch Vehicle; Less Drag; Optimization; Machine Learning; Aerospace

The rocket nose-cone shapes have been generated by blending few conic sections together (two conic sections in one) and the simulated against mach number regime from subsonic through transonic to supersonic. The aerodynamic drag coefficients have been recoded for each shape for each mach number.