Ilyushin TsKB-26 / TsKB-30 / DB-3 / IL-4

The TsKB-26 long-range bomber prototype first flew in 1935, a twin-engined metal low-wing monoplane powered by 597kW Gnome-Rhone K14 radials. Demonstrated by test pilot Vladimir Kokkinaki on May Day 1936, the prototype went on to establish two world altitude records during July 1936.

Ilyushin Il-4 Article

A second prototype, the TsKB-30 had an enclosed instead of open position for the pilot, Soviet M-85 engines and a metal rear fuselage. The TsKB-30 also broke records and then attracted world interest by flying from Moscow to Canada, where pilot Kokkinaki had to make a wheels up landing on 28 April 1939 after covering a distance of 8000km.

DB-3

The TsKB-30 entered production in 1937 as the DB-3B (DB being a Soviet contraction denoting long range bomber). Early examples were powered by 571kW M-85 engines, but these were replaced by 716kW M-86s in 1938.
It served widely with the ADD (Long-Range Aviation) and the V-MF (Naval Aviation), remaining operational well into the war with Germany, DB-3s being credited with some of the earliest attacks on Berlin.
The aircraft suffered from a poor defensive armament of single nose, dorsal and ventral 7.62mm guns, and lost heavily during the Winter War against Finland in 1939-40.

The DB-3 served also with the Finnish air arm between 1940 and 1945, five captured aircraft being augmented by six purchased from German war booty supplies. DB-3 production terminated in 1940 with the 1,528th machine.

In 1939 a modified version with lengthened nose and more armour (the DB-3F) appeared, and in 1940, in conformity with changed Russian practice, the designation became IL-4 (denoting the designer, Sergei Ilyushin).

Il-4

Soon after the German attack on the USSR opened in 1941 it was decided to withdraw IL-4 production to newly opening plants in Siberia, at the same time replacing a large proportion of the metal structure by less strategically critical wood. IL-4s also entered service with Soviet Naval Aviation, and it was a naval manned force of these bombers that first raided Berlin from the east on 8 August 1941. Thereafter the IL-4 paid frequent visits to the German capital and other targets in Eastern Europe. In 1944 production ended, although the IL-4 served until the end of the war and afterwards. Apart from increasing the calibre of its guns and giving it a torpedo carrying ability, the IL-4 remained virtually unchanged between 1941 and 1944.

Well over 5,000 IL-4s were produced between 1937 and 1944, the vast majority in the last three years.

Gallery

DB-3M
Engine: 2 x M-87B, 708kW
Max take-off weight: 7660 kg / 16887 lb
Loaded weight: 5270 kg / 11618 lb
Wingspan: 21.44 m / 70 ft 4 in
Length: 14.22 m / 46 ft 8 in
Height: 4.19 m / 13 ft 9 in
Wing area: 65.6 sq.m / 706.11 sq ft
Max. speed: 445 km/h / 277 mph
Ceiling: 9700 m / 31800 ft
Range: 3800 km / 2361 miles
Armament: 3 x 7.62mm machine-guns, 2500kg bombs

Il-4
Engine: 2 x M88B, 810kW
Max take-off weight: 10055 kg / 22168 lb
Empty weight: 5400 kg / 11905 lb
Wingspan: 21.4 m / 70 ft 3 in
Length: 14.8 m / 48 ft 7 in
Height: 4.1 m / 13 ft 5 in
Wing area: 66.7 sq.m / 717.95 sq ft
Max. Speed: 429 km/h / 267 mph
Cruise speed: 340 km/h / 211 mph
Ceiling: 9700 m / 31800 ft
Range w/max.fuel: 3800 km / 2361 miles
Range w/max.payload: 1200 km / 746 miles
Crew: 3-4
Armament: 3-8 machine-guns, 2500kg bombs

DB-3F
Engine: 2 x M-88, 1100 hp
Wingspan: 70 ft 2 in
Length: 47 ft 6 in
Max speed: 265 mph at 20,000 ft
Sevice ceiling: 30,700 ft
Max range: 2500 mi
Armament: 3 x 7.62 mm mg
Bombload: 4400 lb or 1 x 18in torpedo
Crew: 3-4

Il-4 / DB-3F
Payload: 5,500 lb
Cruise speed: 200 kt
Ceiling: 31,800 ft
Range: 2,400 miles
Crew: 3

Il-4

Ilyushin Il-2 / BSh-2 / TsKB-57

The Ilyushin Il-2 origin dates back to the mid-thirties, within the Soviet military criteria of having air support for the operations of the ground forces.

In 1935 a requirement was launched to obtain a ground attack aircraft that was protected, or more specifically a BSh (Bronirovanyi Shturmovik, armored attack aircraft). Finally Sergei Ilyushin’s team was the one that around 1938 developed the Il-2 that was going to be able to perform the functions required.

Ilyushin Il-2 Article

Two prototypes were developed a few months apart, the two-seater TsKB-55, also designated BSh-2 (from Bronirovanni Shturmovik, armoured attacker) by the air force that first flew on October 2, 1939, and the single-seater TsKB-57, which replaced the radio operator with an additional fuel tank. They were equipped with AM-35 and AM-38 engines respectively, with 1,350 and 1,600hp. of power, heavily armed with 20mm ShVAK cannons, machine guns, bombs and rockets and protected with more than 700 kg of armour.

On 12 October 1940 the TsKB-57 took to the air with the more powerful 967kW M-38 engine. This improved machine led to the IL-2 which was just getting into service when the Germans invaded in June 1941.

Serial production was prepared in factories in Moscow, Fili and Voronezh, but when only the first 250 examples had been delivered, the German invasion occurred on June 22, 1941.

The factories in Fili and Voronezh were moved to Kuybishyev, which became the center of production under pressing pressure from the Kremlin to make the model available in mass quantities.

Armament of the original IL-2 was two 20mm ShVAK and two 7.62mm ShKAS guns firing ahead, plus eight 82mm rockets and four 100kg bombs. The need for rear protection resulted in a second crew member being added to man a rear gun, usually a 12.7mm BS, and the forward guns were changed to the hard-hitting 20 or 37mm VYa, and sometimes two of each, in 1942. Bomb load went up to 600kg, including PTAB armour-piercing bombs. The Shturmovik’s weapons could pierce all German armoured vehicles, even the Tiger tank being vulnerable when attacked from the rear.

Il-2I

The aircraft was redesignated Il-2M with the new 1,750hp AM-38F engine, also increasing the armour up to 950 kgs. A new modification was also introduced, which consisted of converting the radio operator into a tail gunner, handling a 12.7mm UBT heavy machine gun, entering into action as of October 1942 under the designation Il-2M3, which was to be finally the main production version.

The Il-2m3 two seat version had a uniform armoured shell entire forward fuselage, with rear fuselage and wings of plywood and other light materials. They carry two 37mm cannon.

In 1943, the Poles were the first foreign operators of the Il-2, followed by the Czechs, Bulgarians, and Yugoslavs.

By the time the Ilyushin Il-10, an improved variant, went into production in August 1944, 36,163 Il-2 Shturmoviks had been delivered. In the postwar period, significant quantities were delivered to China, North Korea, and both Poland and Czechoslovakia produced improvements on the models, adapting them to their requirements. He received the nickname or code name “Bark” by NATO.

The IL-2 remained in operational service in the Soviet Union and with the Air Forces of Czechoslovakia and Poland into the 1950s.

Output averaged 1,200 per month during most of World War II, to give a total of approximately 36,000. When the IL-10 developed version is added the total is reported to amount to 42,330.

Variants:

  • TsKB-55: two-seater prototype.
  • BSh-2: designation of the TsKB-55 in the V-VS.
  • TsKB-57: single-seat prototype.
  • Il-2: production model of the TsKB-57 (1941).
  • Il-2M: single-seat production model with improved armament and engine.
  • Il-2M3: variant similar to the Il-2M but with a tail machine gunner.
  • Il-2T: torpedo version for the Soviet Navy with the capacity to carry a 533mm torpedo.
  • Il-2U or U-Il-2: trainer version with double control.
  • Il-2I: prototype with M-38 radial engine.

Gallery

Engine: 1 x Mikulin AM-38F V-12, 1300kW / 1770 hp
Wingspan: 14.6 m / 47 ft 11 in
Length: 11.6 m / 38 ft 1 in
Wing area: 38.5 sq.m / 414.41 sq ft
Max take-off weight: 5360 kg / 11817 lb
Empty weight: 4200 kg / 9259 lb
Max. speed: 430 km/h / 267 mph at 6560 ft
Cruise speed: 320 km/h / 199 mph
Ceiling: 6000 m / 19700 ft
Range w/max.fuel: 800 km / 497 miles
Range w/max.payload: 600 km / 373 miles
Armament: 2 x 23mm machine-guns, 3 machine-guns, 400-600kg external
Crew: 1-2

l-2M3
Power plant: Mikulin AM-38F, 1,720hp
Wingspan: 14.60 m
Wing area: 38.50 sq.m
Length: 11.65 m
Height: 4.17m
Empty weight: 4,520 kg
Maximum takeoff weight: 6,360 kg
Maximum operating speed: 410 km/h (255 mph; 221 kt)
Service ceiling: 4,530 m (14,862 ft)
Service ceiling: 4,530 m
Range: 770 km
Wing loading: 160 kg/sq.m
Power/weight: 0.21 kW/kg
Crew: 2
Armament: 2 x VYa-23 23mm mg, 150 rounds per gun, 1 x Berezin UBT 12.7mm machine gun, 150 rounds, 2 x 7.62mm ShKAS machine guns, 750 rounds per gun
Bombload: 50 kg, 100 kg or 200 kg internal
Hard points: 4 / 600 kg total for 2 x Cannon or 2x RS-82 and RS-132 Rockets

Ikarusflug Bodensee Eurofox

Inspired by the Kitfox and Avid Flyer, the Eurofox also uses a welded steel spaceframe fuselage, tubular spars and plywood ribs, all covered in Dacron.

Engine: Rotax 912, 80 hp
Wing span: 9.2 m
Wing area: 11.5 sq.m
MAUW: 450 kg
Empty weight: 250 kg
Fuel capacity: 58 lt
Max speed: 180 kph
Cruise speed: 150 kph
Minimum speed: 60 kph
Climb rate: 5 m/s
Fuel consumption: 10 lt/hr
Certification: VZ
Seats: 2
Price (1998): 63 240 DM

Ikarus Comco C42 / Aerosport Ltd Ikarus C42

The tube and fabric C42 features an unstressed outer skin.
Known as Aerosport Ltd Ikarus C42 in the US, the Ikarus C42 is a popular school plane. More than 650 airplanes have been delivered worldwide.

A newer model is the Ikarus C42B (C-42B). C42B 2009 Price: 40000 EURO

1998

C-42
Engine: Rotax 912, 80 hp
Wing span: 9.9 m
Wing area: 13.2 sq.m
MAUW: 450 kg
Empty weight: 230 kg
Fuel capacity: 50 lt
Max speed: 175 kph
Cruise speed: 150 kph
Minimum speed: 65 kph
Climb rate: 5 m/s
Seats: 2
Fuel consumption: 11 lt/hr

C-42B
Stall: 35 kt / 40 mph / 65 kmh
Cruise: 86 kt / 99 mph / 160 kmh
VNE: 103 kt / 118 mph / 190 kmh
Empty Weight: 259 kg / 572 lbs
MTOW Weight: 450 kg / 992 lbs
Climb Ratio: 1000 ft/min / 5 m/s
Glide Ratio: 1:11 @ 70kn
Take-off distance (50ft obstacle): 1050 ft / 320 m
Landing distance (50ft obstacle): 770 ft / 234 m

C42FB

Ikarus AD J-451MM Stršljen

The J-451MM Stršljen is a development of the single seat 451M Zolja research aircraft, which was the first jet aircraft designed in Yugoslavia.

Ikarus J 451 MM Strsljen

The Ikarus J-451MM Stršljen (“Hornet”) was developed in 1956 as a planned close support variant of the S-451M Zolja and test flown in 1957 by the Aeronautical Testing Centre. The design featured a tricycle undercarriage as opposed to the early tail dragger designs, more powerful Turbomeca Marboré turbojet engines and armament of 2 x 20mm Hispano-Suiza 404A cannons under the fuselage along with underwing rockets.

Ikarus J-451MM Stršljen (“Hornet”)

The airframe has low-set wings without sweepback, and un-swept tail surfaces, with the tailplane mounted part-way up the fin. The ailerons, elevators and rudder are conventional. The wingtips are turned down and a stabilising fin is under the nose. The outer wings fold upward for stowage and access to the engines.

The tricycle undercarriage has single wheels on each unit. The main wheels retract inward and nosewheel retracts forward.

Two cannon are located in fairings under the fuselage and underwing attachments hold up to four air-to-ground rockets.

Engines: 2 x Turbomeca Marbore, 880 lb
Wingspan: 25 ft 10.5 in
Wing area: 121.5 sq.ft
Length: 26 ft 3 in
Height: 5 ft 6 in
Empty weight: 5370 lb
Max speed: 497 mph at SL
Service ceiling: 39,600 ft
Range: 470 mi
Armament: 2 x 20 mm Hispano cannon
Hardpoints: 4

Ikarus AD 215

Originally designed before the World War II as a Zmaj R-1 the Ikarus 215 (Икарус 215 in Serbian) twin-engine plane, was a Yugoslav light bomber and a training aircraft. It was designed by Dusan Stankov and built at the Ikarus factory in Zemun-Belgrade.

The aircraft was of mixed construction, twin engine, with a crew of two to four. The main landing gear wheels retracted rearwards into the motor housing.

The prototype first flew in 1949. The 215 did not enter production. The prototype was used for training.

Engines: 2 × Ranger, SGV-770C-1, 387.7 kW (519.9 hp)
Propellers: 2-blade
Wingspan: 16.14 m (52 ft 11 in)
Wing area: 29.80 sq.m (320.8 sq ft)
Length: 13.35 m (43 ft 10 in)
Height: 4.03 m (13 ft 3 in)
Empty weight: 4,297 kg (9,473 lb)
Gross weight: 4,685 kg (10,329 lb)
Range: 1,120 km (696 mi; 605 nmi)
Service ceiling: 8,150 m (26,739 ft)
Crew: 2-4