Here's something :
www.buran.ru...
www.buran.ru...
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Specs :
Take of engine power, kg - 6x40000
Maximum payload (incl. suspension elements), t - 450
Take off mass, t - 900
Maximum fuel reserve, t - 358
Wing span, m - 90.4
Length, m - 73.4
Maximum cargo dimensions, m:
length - 60
width - 11
height - 9.4
Operational range, km:
with maximum payload - 2300...3100
with maximum fuel reserve - 8300...11800
Cruising speed, km/h: - 840
Take-off run, m - 2350
Landing run, m - 1000
Crew No. of persons:
Basic - 4
shift - 4
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^^ NPO Molniya's proposed stuff
linkAt present NPO MOLNIYA is working not only in the space field but also on aircraft
engineering. A series of civil aircraft with carrying capacity from 500 kgs up to 5 tons are being designed here. To appear on the world market of
such engineering, where extremely rigid competition exists, is possible only with the products appreciably distinguished from the similar ones by
their characte-ristics. Considering this NPO MOLNIYA has chosen a "triplane" aerodynamic scheme stipulating in comparison with traditional schemes
the essential increase of flying safety and fuel economy of its aircraft.
The triplanes have advantages of canard and classical schemes, but are free from their faults. The use of all three planes carrying properties reduces
loads on the construction providing significant (up to 20%) reduction of the aircraft weight and dimensions and therefore the reduction of fuel
consumption and the whole vehicle cost. Besides the triplanes have the following advantages:
the increased level of flying safety because at a high angle of attack a flow separation occurs on the foreplane prior to that on the main wing, that
practically excludes the stall into a spin
the simplicity and easiness of the aircraft pilotage because of small loads on controls
the high lift-drag ratio in cruise flying mode and the improvement of take-of-landing performance stipulated by the reduction of aerodynamic balancing
losses