Identical? No. On is a delta and one is a delta with a square wing placed behind the AC that pivots. As for WIG? You be the judge.
it seems to me interestinglyEarly in the program somebody realized that the plane was capable of floating on its sealed, foam-filled wing. Tests with scale models showed that the airplane could take-off and land on water with the help of hydro-skis. This opened up the possibility of snow landings as well. With retractable skis, the Two-l75 would certainly have had the cleanest seaplane configuration ever seen.
I am ready to help in this caseqxev,
Have them email me and we can get a design that would work for the USA and Russian markets and make some money. Must be roadable, though...
Equipment by easily demountable wings should be feature. should be stored in the closed trailer that allows to save hundreds dollars on collecting the airport storages,
Maximum take-off weight of 700 kg
Maximum pay load of 210 kg
Cruiser speed of 250 km/h
Maximum speed of horizontal flight of 300 km/h
Length of running start of 100 m
Rotax engines of 912ULS 2x100 hp.
Fuel consumption of 18 l/h
Range of reracing 2200 km
Reserved fuels of 200 l
The area covered 10 sq.m
Number of places 1 + 2
Scope of a wing, m 10.00
Length of the plane, m 6.39
Height of the plane, m 1.40
The area covered, sq.m 12.44
normal take-off 560
PD Rotax 912 A3 engine 1 type
Capacity, h.p. 1 x 79
Maximum speed, km/h 165
Cruiser speed, km/h 120-160
Reracing range, km 850
Practical range, km 500
Practical ceiling, m 3000
Crew, person 2
Useful loading: to 90 kg of cargo
I carefully collect, and I analyze information on any new planeqxev,
What relation do you have to this airplane?
it is work of other group... the plane never flied. the model is made onlyWho makes it.
What is the purpose of the design?
attempt to use effect "a circular wing of a kaster"Why the wing bend?
it is too much high technologies... new materials for the chassis are necessary (durability and elasticity) process of operational development will be long and painfulDo you think it has a future? (My answer is no)
this plane, just as ELA-13M tries to use "Brunelli's bearing fuselage"...,qxev,
What is the mission of this airplane? How is it useful other than water landings?
landing speed of 65 kilometers per hourlandings Speed: 35 knots | 40 miles / h | 65 kilometers per hour
Cruise: 81 knots | 93 miles / h | 150 kilometers per hour
AEVVP: 113 knots | 130 miles / h | 210 kilometers per hour
VPP, on 50 foots (15 m) an obstacle: 490 foots | 150 mposadochny distance over 50 foots (15 m) obstacle: 490 foots | 150 m Max. take-off weight: 300 kg | 661 pounds Empty weight: 205 kg | 452 funtovdvigatel: 50 h.p. Fuel consumption: 12 l /
. revolutionary design.
. new category of the planes combining qualities of the scheme «a bearing fuselage (FFA)», «a flying wing (FBA)»