Ilyushin IL-20

Purpose: To design an improved Shturmovik attack aircraft.

Design Bureau: OKB of Sergei Ilyushin, Moscow.

In the Great Patriotic War Ilyushin became fa­mous, even outside the Soviet Union, mainly because of his IL-2 Shturmovik (assaulter). No fewer than 36,163 were delivered, the greatest production run of any single type of aircraft. One reason why so many were need­ed was that attrition was severe, despite their heavy armour. With the IL-10M Ilyushin frac­tionally improved flight performance, and by 1945 the availability of more powerful en­gines opened the way to a further increase in gross weight. In turn this made it possible to rethink the armament, in particular adding a more effective rear defence. The single IL-20 – dubbed Gorboon, hunchback – began flight testing in 1948, but by this time piston-en­gined aircraft for front-line use were becom­ing outdated. Ilyushin dropped the IL-20 and began work on the IL-40 twin-jet Shturmovik, as well as jet bombers and other types.

Ilyushin IL-20Ilyushin IL-20Подпись: Top: IL-20. Above: IL-20 armament. Right: IL-20 pilot view. Ilyushin IL-20The IL-20 was a direct extrapolation of the IL-10 and related types, with similar all-metal stressed-skin construction. A basic shortcom­ing of the wartime Shturmoviks had been that, in most low-level attacks with bombs, the target disappeared under the nose before the bombs could be released. Ilyushin had spent much time trying to devise ways of giv­ing the pilot a better forward view. In 1942 he had tried putting the pilot in the nose, with a shaft drive from an engine behind the cock­pit, but dropped this idea. Various laborato­ries also failed to find good answers, one being the PSh periscopic sight. In 1946 he tried the even more unusual scheme of putting the pilot directly above the engine. The latter was an AM-47F (also called MF-47) liquid-cooled V-12, the last of Mikulin’s big piston engines, rated at 3,100hp, driving a 3.2m (10ft 6in) four-blade propeller. Despite being protected below by armour and with the cockpit above, the engine was said to be readily accessible and removable. The pilot had a cockpit with armour 6 to 9mm thick, with a field of view directly ahead up to 37° downwards, so that in a shallow dive he had a perfect view of the target. Behind the cock­pit was a large protected tank, and behind that a radio operator in a powered turret with an NR-23 cannon. The main landing gears re­tracted aft in the usual manner, the wheels ro­tating 90° to lie flat in the wings. Immediately outboard of these were four NS-23 cannon firing ahead. In one scheme; illustrated on this page, two further NS-23 were fixed obliquely in the rear fuselage firing ahead and

Ilyushin IL-20

downwards. A bomb load of up to 1,190kg (2,623.5 Ib) could be carried in wing cells, and wing racks were provided for eight RS-82 or four RS-132 rockets. There was also to have been an anti-submarine version, never built.

Though clearly a formidable aircraft, the IL-20 actually had a flight performance in almost all respects inferior to that of the wartime IL-10. Ilyushin was certainly right to abandon it, and in fact the basic attack role was later assumed by the simple MiG-15 single-seat fast jet.

Dimensions

Span

17.0m

55 ft 9 in

Length

12.59m

41 ft 3% in

Wing area

44.0m2

474 ft2

Weights

Empty

7,535 kg

16,612 Ib

Fuel/oil

800+80 kg

1,764+176 Ib

Loaded normal

9,500kg

20,944 Ib

Maximum

9,820 kg

21,6491b

Performance

Maximum speed

at sea level

450 km/h

280 mph

at 2,800m (9, 186 ft)

515km/h

320 mph

Time to climb to 3,000 m

8min

9,843 ft

to 5,000 m

12.5min

16,404ft

Service ceiling

7,750m

25,430ft

Range (normal gross weight) 1,180 km

733 miles

(maximum weight)

1,680km

1,044 miles

Take-off run

500m

1,640ft

Landing speed

150 km/h

93 mph

 

Three views of IL-20.