From the start of
Eastern Front combat in World War II, the
Soviet Air Force (VVS) used the successful ground attack aircraft
Ilyushin Il-2 Sturmovik, powered by the
Mikulin AM-38 inline engine. As the war progressed, the Soviets laid plans for that aircraft's successor. The main goal was to increase speed and maneuverability at low altitudes, mainly to evade small-caliber
anti-aircraft artillery, which was the main threat for ground attack aircraft, and to remove some of the Il-2's faults. The most promising project was a modern, light and maneuverable close assault aircraft, the
Sukhoi Su-6, developed by
Pavel Sukhoi's bureau from
1942. At the same time,
Sergei Ilyushin developed a heavier aircraft, the
BSh M-71, (
Il-8 M-71), derived from the Il-2 design, on which it was partly based, to be powered by the prototype
Tumansky M-71 radial engine, which did not enter production. In
1943, Ilyushin started work on a new aircraft,
Il-1, which was to be a 1- or 2-seat
heavily armoured fighter-interceptor, meant mainly for fighting enemy
bombers and transports. The Il-1 was similar to the Il-2 design, but was more modern, compact, and powered with a new Mikulin engine: the AM-42. But the VVS gave up the idea of heavy armoured fighters, due to their low speed, which was not enough to
intercept modern bombers. As a result, Ilyushin decided to turn the Il-1 into a two-seat ground attack plane, with the designation changed to
Il-10 in early 1944 (odd numbers were reserved for fighters). At that time, Ilyushin also finished a
prototype of a heavier ground attack plane, the
Il-8, using the same engine, and more closely derived from the Il-2. It carried a higher payload (), but had lower performance than the Il-10. Both types first flew in April 1944, the Il-10 proving greatly superior to the Il-8, which had poor handling. The Il-10 successfully passed trials in early June 1944. The third competitor was a new variant of the Sukhoi Su-6, also powered by the AM-42 engine. After comparative tests, the Il-10 was considered the winner and was chosen as the new ground attack plane, despite some opinions that the Su-6 was a better aircraft, notwithstanding inferior performance and payload, with better gun armament. Notably, the Su-6 prototype was tested with maximum payload, causing lowered performance, while the Il-10 was tested with normal payload. Some advantages of the Il-10 came from its technical similarity to the Il-2.
Production On 23 August 1944 the Il-10 was ordered into serial production by decision of the State Defense Committee (GKO) as a new ground attack plane. Its armament was initially similar to late model Il-2s, with two
VYa-23 cannons and two
ShKAS machine guns in the wings, and a
UBT machine gun for a rear
gunner, and , or a maximum of bombs. Unlike the Il-2 and Su-6, it was not initially meant to carry
rockets. Production of the Il-10 started in
Kuybyshev's factories No. 1 and No. 18. The first production aircraft flew on 27 September 1944 and 99 aircraft were produced by the end of 1944. Early series aircraft showed teething problems, most notably engine faults and fires. Most problems were eliminated by 1945. Aircraft produced from April 1945 onwards could carry four unguided
air-to-ground rockets. Aircraft produced from 1947 onwards were fitted with stronger armament, consisting of four 23 mm
NS-23 cannons in the wings and a 20 mm cannon for the rear gunner. Il-10 production ended in 1949, after a run of 4,600 aircraft; in the last two years, they were produced in factory No. 64. Between 1945 and 1947, 280
UIl-2 or
Il-10U trainer variants were produced. The rear gunner' cockpit was replaced with a longer instructor's cockpit with dual controls. Its performance and construction were similar to the combat variant apart from armament, which was reduced to two cannons, two rockets, and a standard load of bombs. In 1951, the
Czechoslovak firm
Avia secured a license to make Il-10s, with the designation
B-33. The first one flew on 26 December 1951. Initially, their engines were Soviet-built. From 1952 onwards the engines were also produced in Czechoslovakia as the M-42. Besides the combat variant, a Czechoslovak trainer variant also entered service under the designation
CB-33. In total, 1,200 B-33s were built by 1956. In 1951, due to experience acquired during the
Korean War, the Soviet Air Force decided that
propeller ground attack aircraft might still be useful, and decided to renew Il-10 production in a modified variant, the
Il-10M, which first flew on 2 July 1951. It was slightly longer, with a wider wingspan, and larger control surfaces, with a fin under the tail. Four of the more recently developed
NR-23 cannons were mounted in the wings, while the payload stayed the same, and newer navigation equipment was installed, giving partial all-weather capability. Speed decreased slightly, but handling improved. Between 1953 and 1954, 146 Il-10Ms were made, all but 10 in
Rostov-on-Don's factory No.168. In total, 6,166 of all Il-10 variants were made, including those built under license. Trials of Il-10s mounted with more powerful AM-43 and AM-45 engines took place, but proved unsuccessful. Ilyushin next designed a lighter
close support aircraft, the
Il-16, with improved performance and similar armament. It first flew on 10 June 1945. A short run entered production, but the project was cancelled in 1946 due to the AM-43 engine's unreliability. ==Design==