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The through optimization of fail-safe branched injection trajectories of launch vehicles in view of aerodynamic load constraints on the basis of the maximum principle https://doi.org/10.1051/eucass/201306569
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The through optimization of fail-safe branched injection trajectories of launch vehicles in view of aerodynamic load constraints on the basis of the maximum principle https://doi.org/10.1051/eucass/201306569
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