680394.fig.002a
(a)
680394.fig.002b
(b)
680394.fig.002c
(c)
680394.fig.002d
(d)
680394.fig.002e
(e)
Figure 2: Reduced flow ( 𝑟 , 𝑅 ) of the constant propulsive acceleration problem in the parameters ( , Θ 2 ) -plane.