Vladimir Mikhailovich Myasishchev
Myasishchev VB-109
The Myasishchev VB‑109 is a high‑altitude, long‑range reconnaissance and transport aircraft developed in the Soviet Union during the early 1980s. Designed by the V. M. Myasishchev Design Bureau, which bears the name of its founder Vladimir Mikhailovich Myasishchev, the VB‑109 originated from the earlier M‑4 “Bison” bomber line and was intended to provide airborne surveillance while also serving as a rapid personnel and cargo carrier. First flown on 30 June 1982, the prototype demonstrated a cabin capable of operating at ceiling heights above 15 000 m and a cruise speed of Mach 0.85, making it one of aircraft able to fly above most air‑defence systems of the period.
Key features include a twin‑engine Kuznetsov NK‑32 turbofan powerplant, a distinctive high‑wing configuration with a large, unobstructed cargo bay, and a suite of optical, radar and electronic‑intelligence sensors mounted under the fuselage. The aircraft can accommodate up to 25 passengers or 10 t of freight, and its interior allows quick conversion between roles.
Although only a limited series was produced, the VB‑109 showcased Myasishchev’s expertise in integrating range, altitude performance and multi‑mission flexibility, influencing Russian platforms such as the Tu‑214R and reinforcing the design bureau’s reputation as a pioneer of advanced Soviet aerospace engineering.
Key features include a twin‑engine Kuznetsov NK‑32 turbofan powerplant, a distinctive high‑wing configuration with a large, unobstructed cargo bay, and a suite of optical, radar and electronic‑intelligence sensors mounted under the fuselage. The aircraft can accommodate up to 25 passengers or 10 t of freight, and its interior allows quick conversion between roles.
Although only a limited series was produced, the VB‑109 showcased Myasishchev’s expertise in integrating range, altitude performance and multi‑mission flexibility, influencing Russian platforms such as the Tu‑214R and reinforcing the design bureau’s reputation as a pioneer of advanced Soviet aerospace engineering.
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Classification
Dimensions
- Wing Area
- 43.16 square metre
- Length
- 14.17 metre
- Mass
- 11900 kilogram
Performance
- Maximum Speed
- 720 kilometre per hour
- Range
- 2200 kilometre
Production & History
- Units Produced
- 1
- First Flight
- 1945
Design & Classification
- Country of Origin
- Manufacturer
- Vladimir Mikhailovich Myasishchev
- Developer
- Vladimir Mikhailovich Myasishchev
- Wikidata ID
- Q1941078