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In early Soyuz models there were two abort modes in the time ranging from the ejection of the launch escape system until orbit. One called for separation of only the upper two modules and a controlled descent and could be initiated before about T+522s, the other separated all three and underwent a ballistic descent after T+522.<ref name = 'hall & shayler'>{{cite book|last1=Hall|first1=Rex|last2=Shayler|first2=David J.|title=Soyuz: A Universal Spacecraft|date=2003|publisher=Praxis Publishing Ltd.|location=Chichester, UK|isbn=1-85233-657-9|page=70|url=https://books.google.com/books?id=dbGchpi1HP8C&pg=PA67}}</ref>
Unlike the [[
==Reliability==
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