The drag power is plotted per frontal surface area of a capsule moving at subsonic (1,000 km/h) and transonic (1,235 km/h), respectively. The projections are calculated from the drag equation (Fd = 0.5*Cd*rho*A*v2), where the drag power (or air loss) is the drag force (Fd) times the speed (assuming a unitary drag coefficient, Cd = 1). Ideal gas law (p = RT*rho) is used to obtain the air density (rho) as a function of both pressure (p) and temperature (T ), where R = 287.05 J/kgK.

The drag power is plotted per frontal surface area of a capsule moving at subsonic (1,000 km/h) and transonic (1,235 km/h), respectively. The projections are calculated from the drag equation (Fd = 0.5*Cd*rho*A*v2), where the drag power (or air loss) is the drag force (Fd) times the speed (assuming a unitary drag coefficient, Cd = 1). Ideal gas law (p = RT*rho) is used to obtain the air density (rho) as a function of both pressure (p) and temperature (T ), where R = 287.05 J/kgK.

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