Assertion: turbine's thrust | /r/CapableOf | go in 1990
Facets:
value: to 115,000 lbf
type: OTHER
Source sentences:
text: The thrust of a typical jetliner engine went from 5,000 lbf (22,000 N) (de Havilland Ghost turbojet) in the 1950s to 115,000 lbf (510,000 N) (General Electric GE90 turbofan) in the 1990s, and their reliability went from 40 in-flight shutdowns per 100,000 engine flight hours to less than 1 per 100,000 in the late 1990s.