FIELD: aeronautical engineering. SUBSTANCE: ramjet engine is mounted in nacelle 1 located under wing 2; it includes housing 3 of rectangular cross section with outer gas compression panel 4 and gas expansion panel 5, combustion chamber panel 6, side vertical walls and movable ferrule 8. EFFECT: enhanced reliability. 17 dwg
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Authors
Dates
1998-02-10—Published
1992-04-24—Filed