FIELD: aeronautical engineering; ejection systems.
SUBSTANCE: twin ejection is carried out by means of ejection system including three pyro-mechanisms mounted on one of ejection seats; one pyro-mechanism actuates pyro-cylinder of other seat through gas duct feeding pulse to its ejection drive. Two other pyro-mechanisms actuate at time delay pyro-cylinder feeding pulse to ejection drive of first ejection seat.
EFFECT: simplification of system; enhanced reliability and self-containment due to use of pyro-system.
1 dwg
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Authors
Dates
2006-10-27—Published
2005-03-03—Filed