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As a mission planner, I can straightforwardly compute accelerations involving multiple stages. Currently, multi-stage accelerations can be computed by manually changing the payload mass between acceleration phases.
The text was updated successfully, but these errors were encountered:
As a mission planner, I can straightforwardly compute accelerations involving multiple stages. Currently, multi-stage accelerations can be computed by manually changing the payload mass between acceleration phases.
The text was updated successfully, but these errors were encountered: