Space: Science & Technology / 2022 / Article / Tab 1

Research Article

Study on Effect of Aerodynamic Configuration on Aerodynamic Performance of Mars Ascent Vehicles

Table 1

Incoming flow conditions for MSL supersonic aerodynamic calculation.

(°) (m/s) (kg/m3) (K)

2.090, 6, 11, 16, 20, 24472190.21.24822