FIELD: aeronautical engineering.
SUBSTANCE: proposed aircraft is provided with main power plant including supersonic engines, additional power plant located in lower section of fuselage behind crew cabin and integral complex of onboard radio electronic equipment , aircraft complex control system, shipboard equipment control system, aircraft complex power supply system, electronic display complex and self-contained onboard oxygen system. Proposed aircraft may be used under varying flight conditions including conditions of using autonomous home airfield in case of separation from main airfield.
EFFECT: enhanced efficiency.
3 cl, 15 dwg
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Authors
Dates
2006-03-10—Published
2004-11-05—Filed