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Apollo abort modes
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== Mode V == A Mode V abort was only planned for use during the [[Apollo-Soyuz Test Project]] launch. In the event of an early S-IVB shutdown, the CSM RCS thrusters would be used to insert the entire stack (including the docking adapter) into orbit. The time window for a Mode V abort was only 1.5 seconds before nominal S-IVB cutoff.
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