They came in at the top five. At the center of the Su-34 and on the sides of the 4 su-27. Su-34 with tail number 28.
made a circle group
and started to go to the cloud
The chief designer of the two-seater fighter-bomber with the initial designation of the Su-27IB (factory code of the T-10B) was appointed R.G. Martirosov, general management was headed by General Designer MP Simonov.
The design and refinement of one of the serial Su-27UBs to the prototype of the T-10B-1 fighter-bomber were completed, mainly by 1990. The 42 vehicle serial number was a serial “split”, in which the standard fuselage head was replaced The new two-seater cabin and entrance through the niche of the front landing gear, the new influx of wing and other changes according to the project fighter-bomber.
The first flight of the prototype, which was piloted by Honored Test Pilot A.A. Ivanov, took place at 13.04.1990 at the airfield of LII. M.M.Gromova. Subsequently, comprehensive tests of the aircraft with the new head of the fuselage, air refueling, and other studies took place.
For serial production of a new aircraft was elected NAPO them. V.P. Chkalov, previously known as Plant No. 153 and Novosibirsk aviation factory (NAZ). The first aircraft was built in late autumn 1993, and on December 18, test pilots I.V. Votintsev and E.G. Revunov took it on their first flight, accompanied by a Su-24 bomber with a crew of test pilots E.N. Rudakas and A.I. Gaivoronsky.
In 1995, the repainted Su-34 with tail number 45 was presented at the international air show in Le Bourget (France) under the name Su-32FN (Fighter Navy - naval fighter). It was the third name of the same aircraft (the customer still calls it Su-27IB, development company - Su-34, abroad - Su-32, at the factory - T-10B).
To date, it seems like 7 prototypes and 46 production aircraft have been produced. Perhaps already more. Unit cost 1,05 billion rubles (~ $ 32 million)
The new Su-34 is intended to replace the older Su-24 bombers.
12 and 22 December 2011 of the year six new Su-34 bombers arrived at the Baltimore Air Force Base in Voronezh, so this base became the first Air Force unit to receive these machines, and from there it came to us.
near the fire brigade ponabilos workers with relatives look at MAKS
here and children and barbecue !!!
And here on the next pass the planes diverge.
Four Su-27 goes to the waiting area
and Su-34 goes to the loop
The aircraft is piloted by Alexander Nikolaevich Kharchevsky (born 9 in May 1950) - Head of 4 of the State Center for Training of Aviation Personnel and Military Tests (Lipetsk). Lead aerobatic team "Falcons of Russia". Honored Military Pilot of the Russian Federation, Major General Aviation. Former Head of the Military Training and Scientific Center of the Air Force “Air Force Academy named after Professor N. Ye. Zhukovsky and Yu. A. Gagarin” (Voronezh) - VUNC VVS Air Force (Voronezh) in Voronezh and 4 Center for combat use and retraining of flight personnel.
And you in 63, the year is a little sculpt in the air?
at the top of the coup, all in the cloud
and again on us
above us goes up
what curls :-))
and then the barrel
the weather did not dispose to normal photography, and in normal weather they did not get to me. From here I leave it as a nick in the memory-it was ...
here you can look at the aerodynamics of the aircraft in all its glory
I'm going to you ...
is it in the afterburner such an exhaust orange?
and again breakdowns
Different options apparently from the angle of attack?
I have the impression that the front wings at almost all stages of the flight down rejected?
and call on us again
up with rotation
smooth bottom view
and here so
Aircraft continue to fully develop and modernize.
After that, he left, and he was replaced by four Su-27, but this is a separate story.
Crew: 2 person
Length: 23,3 m
Wingspan: 14,7 m
Height: 6,0 m
Wing area: 62 m²
Sweep angle: 42 °
Wing Extension Ratio: 3,5
Chassis base: 6,63
Track Chassis: 4,4 m
empty: 22500 kg
normal takeoff: 38240 kg
maximum take-off: 45000 kg
Engine: 2 × TRDDF AL-31F-М1
maximum speedless: 2 × 8250 kgf
afterburner: 2 × 13500 kg
Bypass ratio: 0,571
Engine weight: 2 × 1520 kg
Maximum operating overload: + 7G
at the ground: 1400 km / h
at high altitude: 1900 km / h (1,8M)
Range of flight: 4000 km
Breakout speed: n / d
Landing speed: n / d
Combat radius: 1100 km
Service ceiling: 17000 m
with normal take-off weight: 616 kg / m²
with maximum take-off weight: 725 kg / m²
normal take-off weight: 0,71
with maximum take-off weight: 0,6
Cannon armament: 1 × 30 mm gun GSH-30-1
Suspension points: 12
Combat load: 8000 kg of various weapons on the external load