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Soyuz abort modes: Difference between revisions





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| 26 September 1983 || [[Soyuz 7K-ST No.16L|Soyuz T-10-1]] || The rocket caught fire on the pad. The launch escape system was fired, pulling the spacecraft free two seconds before the rocket exploded. This is, to date, the only successful manned [[pad abort test|pad abort]].<ref name="JANE">{{cite web|url=http://www.janes.com/aerospace/civil/news/jsd/jsd030203_3_n.shtml|title=A brief history of space accidents|publisher=[[Jane's Information Group|Jane's Transport Business News]]|archiveurl=https://web.archive.org/web/20030204073904/http://www.janes.com/aerospace/civil/news/jsd/jsd030203_3_n.shtml|date=February 3, 2003|archivedate=2003-02-04|accessdate=2007-10-20}}</ref>
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| 11 October 2018 || [[Soyuz MS-10]] || The [[Soyuz-FG]] booster failed around booster separation. Back-up Themotors launchon escapethe systemcapsule fairing pulled the spacecraft free of the rocket.<ref>{{cite news |last1=Gebhardt |first1=Chris |title=Soyuz FG fails during ascent – Soyuz MS-10 crew safe after ballistic entry abort |url=https://www.nasaspaceflight.com/2018/10/soyuz-reduced-2-crew-launch-station/ |accessdate=10 October 2018 |work=NASASpaceFlight.com}}</ref>
|}
 

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