Research Article

Preliminary Aerodynamic and Aerothermodynamic Assessment of the VTO Hopper Booster

Figure 20

Mach no. contours (a). Normalized pressure contours on vehicle surface (b). Euler computation at 𝑀 = 5 , 𝛼 = 1 0 deg (a) and 𝛼 = 2 0 deg (b).
215785.fig.0020a
(a)
215785.fig.0020b
(b)