Drawings ARGO Aircraft - 02 For Self-built,Plans Cd.

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