AT 1957 g. in EDO AS. Yakovlev, in accordance with the government decree, It began to develop a two-seater initial training of pilots of the Yak-104. Initially, the aircraft engine designed for P-5-45 NG structure. Mechverišvili, but soon, in connection with the cessation of work on the engine, stopped working on it. 31 July 1958 g. There was a new government decree number 854-404 on the construction of the Yak-104, but with the engine design with RU19-300. TO. Tumansky. Airplane Yak-104, subsequently received the designation Yak-30, - this is an all-metal nizkoplan trapezoidal wing and empennage odnokilevym with an average position of the stabilizer.
At the top of the fuselage 30 is Yak-fold gargrot, inside which are laid control and traction electroplaits. In front of the fuselage accommodated equipment units and the pressurized cabin ventilation type with ejection seats with curtain. Rear seat up front on 160 mm to improve the instructor review. Bailouts for the first time in our country could be produced through the glazing, without discharge lamp, when pulling the soft curtain to protect persons. Such a method can reduce the time the emergency evacuation of the airplane. Tricycle landing gear with nose wheel.
The engine is mounted in the middle part of the fuselage. The air intake has two inputs in the wing roots, protected mesh with the side windows of the foreign objects. Engine installation recalls Reda scheme first jet fighters.
Factory tests were carried out on two machines 29 May 1960 g. in March 1961 g. The first flight of an airplane made 2 July 1960 city, He piloted his test pilot VG. Mukhin. Almost in parallel at the same time two sports aircraft were created: Polish TS-11 "Spark" and Czechoslovakian L-29 "Dolphin". On the Monino airfield near Moscow in 1961 g. underwent comparative flight tests of the TS-11 "Iskra", L-29 "dolphins" and our Yak-30. Despite the recommendations of experts take a Yak-30 (the aircraft was flying a positive assessment of all three delegations - USSR, CSSR and Poland), preference was given to L-29 "Dolphin".
In the end of August 1960 g. began public testing of the Yak-30. The aircraft showed the entire complex aerobatics. Successfully passed the bailout test, provides a safe evacuation of the airplane through the glazing. After state tests, in September 1961 city, the second Yak-30 pilot VP. Smirnov two world records were set: rate on the basis of 15-25 km - 767,308 kmh, height - 16 128 m.
4 February 1959 g. the government issued a decree on the construction based on the Yak-30 single version of the aircraft. Only three aircraft were built Yak-32. The aircraft was tested from January 1961 city, and the state have not been conducted.
The Yak-32 three world records were set:
– 22 February 1961 g. - height 14 283 m, Pilot - VG. Mukhin.
– 14 January 1965 g. - speed on a closed route 100 km - 724,430 kmh, pilot - GG. Korchuhanova.
– 19 February 1965 g. - on the basis of the speed of 15-25 km - 755 kmh, Pilot - P.M. Shyhyna.
Tactical-technical characteristics of the Yak-30
– chief designer: KV. Synelschykov
– First flight: 1960 year
– units produced: 4
As the 30 crew
– 2 man
The dimensions of the Yak-30
– Length: 10,14 m
– Wingspan: 9,39 m
– wing area: 14,30 m²
As Wes-30
– empty weight: 1514 kg
– Maximum takeoff: 2400 kg
Engine Yak-30
– 1 Various block-19-300
– pull: 1 x 900
Speed Yak-30
– full speed: 660 kmh
Range of flight of the Yak-30
– 965 km
Practical ceiling Yak-30
– 14000 m
Photo Yak-30
As at 30 aэrodrome Borki
