Yermolayev Yer-2 - Development

Development

Roberto Bartini had designed and built the Stal-7 airliner whilst he was the chief designer at the ZOK NII GVF (Russian: Zavod Opytno Konstrooktorskoye Naoochno-Issledovatel'skiy Institoot Grazdahnskovo Vozdooshnovo Flota — "Factory for Special Construction at the Scientific Test Institute for the Civil Air Fleet"). The performance of the Stal-7 was extremely good, particularly in respect to its payload; at gross overload weight over 56% of the total weight was payload. During flight trials with maximum all-up weight the prototype crashed on take-off in early 1938, resulting in the arrest of Bartini and his imprisonment in a Siberian Gulag in February 1938. The Stal-7 lay unrepaired until Vladimir Yermolaev was appointed as chief designer at OKB-240 after Bartini's arrest, with the task of transforming the Stal-7 design into a long-range bomber, a task made easier since Bartini had reserved space for a bomb bay in the fuselage. After repair the Stal-7 carried on with the flight-test programme, including a record-breaking non-stop flight on 28 August 1939 when it flew Moscow—Sverdlovsk—Sevastopol—Moscow; a distance of 5,086 km (3,160 mi) at an average speed of 405 km/h (252 mph).

Preliminary design of the DB-240 (Russian: dahl'niy bombardirovschik—"long-range bomber"), as the bomber version was designated, was complete by the beginning of 1939 and the construction of two prototypes began the following July. The DB-240 retained little apart from the general layout of the Stal-7 as the structure was almost completely redesigned. The pilot's cockpit was offset to port to improve his downward view and the navigator/bomb aimer sat in the extensively glazed nose with a 7.62-millimeter (0.300 in) ShKAS machine gun, the radio operator sat below and to starboard of the pilot and the dorsal gunner in a partially retractable turret with one 12.7-millimeter (0.50 in) Berezin UBT machine gun. Another ShKAS was fitted in a ventral hatch. Up to 2,000 kg (4,409 lb) of bombs could be carried in the bomb bay and two 500-kilogram (1,102 lb) bombs could be carried externally. Up to 4,600 kg (10,141 lb) of fuel could be carried. The DB-240 had been designed to use the experimental Klimov M-106 V12 engines, but the less-powerful Klimov M-105 engine had to be substituted because the M-106 was not available.

The DB-240 prototype flew for the first time on 14 May 1940 and began its State acceptance tests on 27 September 1940. The weaker engines prevented the DB-240 from reaching its designed performance. It could only attain 445 km/h (277 mph) at 4,250 m (13,944 ft) instead of the expected 500 km/h (311 mph) at 6,000 meters (19,685 ft). Its defensive armament was deemed inadequate and other problems included an excessively long take-off run and engine defects. However, these did not offset its virtues of a heavy bomb load and long-range (4,100 kilometers (2,548 mi) carrying 1,000 kg (2,205 lb) of bombs). It was ordered into production at Factory No. 18, in Voronezh, as the Yermolayev Yer-2.

Manufacture began in March 1941, with approximately 50 aircraft delivered by 22 June 1941. These aircraft were about 5–8 km/h (3.1–5.0 mph) slower than the prototype and their normal weight increased 1,220 kg (2,690 lb) to 12,520 kg (27,602 lb). Production was terminated in August after 128 had been completed to allow the factory to concentrate on the higher-priority Ilyushin Il-2 ground-attack aircraft.

A Yer-2 was modified with experimental Mikulin AM-37 engines, a reinforced undercarriage, armored seats for the navigator and gunner, and 12.7 mm UBT machine guns in place of its original ShKAS weapons. It first flew in July 1941 and was able to reach 505 km/h (314 mph) at 6,000 m (19,685 ft), but the range was reduced to (3,500 km (2,175 mi) carrying 1,000 kg (2,205 lb) of bombs. One significant problem with this version was the excessive take-off roll which hindered operations from grass airstrips. The engine was unreliable, however, and had cooling problems that the Mikulin OKB did not have the resources to resolve so it was cancelled in October when the factory was forced to evacuate from Moscow by the German advance.

The Charomskiy M-40F Diesel engine was also evaluated in a Yer-2 in 1941. This engine, like all Diesels, offered a greatly reduced fuel consumption compared to a standard gasoline-powered engine, but at a great penalty in weight. These engines increased the gross take-off weight to 13,500 kg (29,762 lb) which required the undercarriage to be reinforced and the wing area increased to keep the same wing loading. The M-40F-powered aircraft reached a maximum speed of 430 km/h (267 mph) at 6,050 m (19,849 ft). However, the M-40 was not yet ready for service use and the project was cancelled.

The aircraft/engine combination did have enough potential that development work continued using the closely related, but more mature, Charomskiy ACh-30B Diesel engine. The cockpit was modified to accommodate two pilots side-by-side and the wing and tailplane areas were increased. The 12.7 mm UBT machine gun in the dorsal turret was replaced by a 20-millimeter (0.79 in) ShVAK cannon and the nose and ventral ShKAS machine guns were exchanged for 12.7 mm UBT machine guns. Up to 5,460 kg (12,037 lb) of fuel could be carried. The Yer-2/ACh-30B was placed into production at Factory No. 39 in Irkutsk at the end of 1943 and the first production aircraft was submitted to its State acceptance trials the following month. Some excess aircraft were converted as Yer-2ON VIP transports.