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General information | |
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Type | Heavy lift helicopter |
Manufacturer | Mil Design Bureau |
Status | Prototypes tested, cancelled |
Primary user | Soviet Union |
Number built | 2 |
History | |
First flight | (27 June 1967 – unsuccessful)10 July 1968 – first successful flight |
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Design studies for a giant helicopter were started at the Mil OKB in 1959, receiving official sanction in 1961 by the GKAT (Gosudarstvenny Komitet po Aviatsionnoy Tekhnike - State Committee on Aircraft Technology) instructing Mil to develop a helicopter capable of lifting 20 to 25 tonnes (22 to 28 short tons). The GKAT directive was followed by a more detailed specification for the V-12 with hold dimensions similar to the Antonov An-22, intended to lift major items of combat material as well as 8K67, 8K75 and 8K82 inter-continental ballistic missiles (ICBM).
Design limitations forced Mil to adopt a twin rotor system but design studies of a tandem layout, similar to the Boeing CH-47 Chinook, revealed major problems. The single rotor layouts also studied proved to be non-viable, leading to the transverse layout chosen for the finished article
Ceiling
MAX RANGE
Aircraft Speed
Max Crew
The Soviet made Mil V-12 (Also referred to as the Mi-12, NATO reporting name "Homer") is the largest helicopter ever built. The name "Mi-12" would have been the name for the production helicopter. Since the V-12 never went into production and only two prototypes were built, the name "Mi-12" was never adopted.
The V-12 features the only two-rotor transverse scheme ever built by Mil eliminating the need for a tail rotor.
The Soviet Kamov OKB built an experimental aircraft with the same scheme in 1958, Kamov Ka-22 Vintokryl . This aircraft had also the combined wing/rotor arrangement later used on the Mil V-12.