FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Proposed aircraft comprises fuselage, hypersonic ramjet with nozzle located under fuselage tail bottom panel, wing, keel and air intake arranged under fuselage tail section. Aircraft nose is equipped with wings sliding on rollers for extension from fuselage to compensate for unfavorable moment caused by gas flow from engine nozzle.
EFFECT: better longitudinal stability.
8 dwg
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Authors
Dates
2014-03-10—Published
2012-10-01—Filed