Load factor restriction algorithm at skip-up return trajectory from the Moon
Abstract:
Load factor restriction algorithm at skip-up return trajectory from the Moon is suggested. Reentry trajectories with range of 10000 km und two atmospheric phases are considered. The algorithm that provides load factor not more than 5.7g at both phases is developed.
Keywords:
terminal control, reentry at return from the Moon orbit, skip-up trajectory, restriction of load factor
