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Drawings ARGO aircraft - 02 for self-built,Plans cd.

$ 7.91

Availability: 100 in stock
  • Warranty: 60 Day
  • Country/Region of Manufacture: Kazakhstan
  • Condition: New
  • Returns Accepted: ReturnsNotAccepted

    Description

    Drawings ARGO aircraft - 02 for self-built,Plans
    Drawings
    aircraft
    ARGO
    - in Russian
    .
    You can easily make
    the translation
    into your language.
    One of the simplest and most common aircraft building itself.
    Download drawing Argo 02 aircraft, you can at the bottom of the page.
    "Argo-02" - ultralight trainer classical cantilever monoplane of wooden construction with bottom-wing cantilever and tail.
    The aircraft has a chassis spring type with tail wheel.
    The power plant of the aircraft - a two-stroke twin-cylinder air-cooled engine type RMZ-640, Rotax, which through V-belt gear drives the two-bladed wooden propeller monoblock.
    The control system of the aircraft "Argo-02" - normal type.
    The cockpit is equipped with instruments and aerobatic team of engine control instruments.
    Flight and technical information about aircraft ARGO-02
    Length, m ...... .. 4.55
    Height, m ​​...... .. 1.8
    Wing span, m ... .. 6.3
    Wing area, m2 .... 6.3
    Narrowing wing ......
    0
    End wing chord, m. ... MAR 1.0, 1.0 m .........
    The installation angle of the wing, hail. . .
    4
    Angle V, hail. ....... 4
    Sweep angle, deg. . . 0
    Aerofoil. . P-III-15,5%
    Area aileron m2. . . 0,375
    The scope of the aileron, m.. . . . 1.5
    Aileron angles, degrees .:
    up ...... .. 25
    down ...... .. 16
    Swipe GO m. . . . ,. 1.86
    Area Defense, m2 ...... 1.2
    Installation angle GO degrees. 0 ...
    PB area, m2. . . . . 0.642
    IN area, m2 ... .. 0.66
    IN Height, m. ...... 1.0
    Area ROP m2. . . . . 0.38
    Deflection angle RN, hail. . ± 25
    Deflection angle PB degrees. , ± 25
    The width of the fuselage for the cabin, m. . . . 0.55
    The height of the fuselage for the cabin, m ...... 0.85
    Base wheel chassis, m. . . 2.9 Track chassis, m ...... 1.3
    Powerplant - RMZ-640 engine with a silencer, cooling air
    Power, L. p. ...... 28
    Max, speed, 1 / min ...... .. 5500
    Reducer. . . V-belt, chetyrehruchevy, belts A-710
    Gear ratio .... 0.5
    Fuel ... .. gasoline A-76
    Oil ...... .. MS-20
    Screw diameter, m. . . . . 1.5
    Pitch, 0.95 m ......
    Static thrust, kgf .... 95
    Weight of empty machine kg. . 145
    Maximum take-off weight, kg. . . . . . . . 235
    Fuel capacity, l ...... 15
    Flight range of CG, MAR ...... .. 24 ... 27
    Stall speed, km / h. . 72
    Max speed horizontal flight, km / h ... .. 160
    Max speed piloting km / h ......... 190
    Cruising speed, km / h ... 120
    Lift-off speed, km / h ... 80
    Landing speed, km / h. . 70
    Climb from the earth, m / s .......... 2
    Run, m ...... .. 100
    Mileage, m ...... .. 80
    The range of operating loads. ....
    + -1.5 W ...
    Dimensions in transportation, m ....... 5X2,3X1,8
    Those who decided on the construction of this unit, I can advise the site (blog) guys who are engaged in self-production aircraft Argo-02 http://argo02.h1.ru/
    Fuselage - wood, diagonally - uniform design. Fuselage spars are made of wooden slats section 18X18 mm.
    Here's a link to the video of the finished aircraft.
    http://youtu.be/0HHq8t1WKME
    Files will be sent to the CD drive.