Aviation of Word War II

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Er-2ON


Er-2ON
  • Special purpose transport aircraft
  • Yermolaev

Er-2 ON is a special-purpose transport aircraft. It is reliably known only about one flight of I.V. Stalin by plane, in 1943 to the Tehran conference to meet with F. Roosevelt and W. Churchill. The twin-engine Li-2, specially prepared for this flight, turned out to be the most suitable for this.

However, Li-2 did not meet the requirements of the time in terms of speed, range and flight comfort. Even alterations could not eliminate its shortcomings. And then it was decided to create a special aircraft for the flights of the country's top leadership. By order of NKAP No. 351 dated May 23, 1944, the development of a "special purpose" aircraft was entrusted to the design bureau of V.G. Ermolaev. For the fastest execution of the mission, the aircraft was decided to be built on the basis of the Er-2 bomber under the designation Er-2ON. In addition to excellent flight characteristics, there was another important condition - the aircraft engines ran on heavy diesel fuel, which is much safer in terms of fire safety. Particular attention was paid to the comfort of the passenger compartment, its interior, the convenience of communication between important persons in flight, the aisle for warm-ups, etc. All this was worked out on special full-scale models and was carefully adopted by the commission.

At the same time, similar orders were issued for the alteration of Pe-8 (Pe-8 ON) and B-25C. Despite the "extraordinary" instructions, the construction of the machines was delayed, since in August 1944 they had to go through a mock-up commission, and dangerous defects of the serial ACh-30B diesel engines manufactured at plant No. 500 were revealed, which required unconditional elimination.

N.V. Sinelnikov was appointed the lead engineer for EP-2 ON. All weapons were removed from the plane, and in place of the bomb bay and fuselage tanks, a passenger compartment of increased comfort with nine seats plus a place for a steward was equipped. The crew of the aircraft for special flights was increased: it consisted of the commander, co-pilot, navigator, radio operator and two flight attendants.

Factory tests of the vehicle began in February, and on April 16, 1945, the first Er-2 ON under the control of Alekseev made a successful non-stop flight from Irkutsk to Moscow, in 15 hours 30 minutes. The second such machine was flight tested at the end of April.

Flight tests found that the plane could fly at a speed of 435 kilometers per hour for a range of 5200 km at an altitude of 6000 m. The plane was to be built in small series in Irkutsk, but the death of Ermolaev on the eve of the new 1945 violated these plans.



Er-2ON
Crew 3
Dimensions
Length, m 16.65
Wing span, m 23.01
Wing area, m² 79.10
Weight, kg:
Empty 8,940
Loaded weight 12,670
Powerplant
2 × DE ACh-30B
Takeoff power, h.p. 2 × 1500
Performance
Maximum speed, km / h 455
Cruising speed, km / h 390
Service range, km 5,500
Service ceiling, m 7,500
Payload, passengers: 9

After the death of Ermolaev, his design bureau was merged with the P.O. Sukhoi, where further work was carried out on the special-purpose aircraft. Several machines have been built and tested successfully. It was only required to bring its highly economical diesel engines to the calculated resource. However, the OKB P.O. Sukhoi, engaged in the development of fighters, was not interested in the subject inherited "by inheritance." Gradually, the work was curtailed.

Photo Description
Drawing Er-2

Drawing Er-2

Bibliography

  • "The history of designs of planes in USSR 1938-1950" /Vadim Shavrov/
  • "Avia Master # 2 1999 " /Al. Medved, Dm. Khazanov/
  • "Planes of Stalin falcons" /Konstantin Kosminkov and Dmitriy Grinyuk/