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If the rocket failed during the first phases of the flight, the [[Emergency Detection System]] (EDS) would automatically give the command to abort. The reason is that life-threatening situations can develop too fast for humans to discuss and react to. In the later, less violent phases of the ascent, the EDS was turned off and an abort would have to be initiated manually.

If the rocket failed during the first phases of the flight, the [[Emergency Detection System]] (EDS) would automatically give the command to abort. The reason is that life-threatening situations can develop too fast for humans to discuss and react to. In the later, less violent phases of the ascent, the EDS was turned off and an abort would have to be initiated manually.


However, while almost all failures were covered, analysis showed that not all failure modes were survivable, notably, an unexpected explosion on the pad could throw debris from the first stage though the command module before escape was possible, inspite of the relatively large distances involved. This was not discussed with the crew.



==Overview==

==Overview==

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