Figure 9.
PE transmission loss predictions at a frequency of 2.0 Hz for Artemis and Apollo (top and bottom rows, respectively) using flat ground (left column) and realistic terrain (right column). These PE simulations are done via an N × 2D approach in which each azimuthal range-altitude slice is computed independently.

PE transmission loss predictions at a frequency of 2.0 Hz for Artemis and Apollo (top and bottom rows, respectively) using flat ground (left column) and realistic terrain (right column). These PE simulations are done via an N × 2D approach in which each azimuthal range-altitude slice is computed independently.

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