Research Article

Preliminary Aerodynamic and Aerothermodynamic Assessment of the VTO Hopper Booster

Figure 21

Pressure coefficient contours on vehicle surface with 3D streamtraces (left side). Mach no. contours on different cross planes. Euler computation at 𝑀 = 1 0 , 𝛼 = 2 0 deg.
215785.fig.0021a
(a)
215785.fig.0021b
(b)