Application of Periapse Maps for the Design of Trajectories Near the Smaller Primary in Multi-Body Regimes

Figure 7

Comparison of periapse maps for different Jacobi values and different systems.

(a) Sun-Saturn escape map for six periapses at a value of Jacobi constant 𝐶=3.0174

(b) Earth-Moon escape map for six periapses at a value of Jacobi constant 𝐶=3.17212

(c) Sun-Saturn sequence originates with Π_𝐿^𝑡+_1,6 through Π_𝐿^𝑡+_1,1 to escape through the 𝐿₁ gateway

(d) Earth-Moon sequence originates with Π_𝐿^𝑡+_1,6 to escape through the 𝐿₁ gateway