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Military


Tu-111

In 1954 in the OKB AN. Tupolev made preliminary studies on a 24-passenger passenger aircraft Tu-111 with two turboprop engines such as TV-2M. The Tu-111 was a twin-engine low-wing with a straight wing, a normal tail unit and a three-wheeled chassis with a nose wheel. The entire stock of fuel was mixed in the wing. The passenger cabin was sealed with a toilet and a capacious luggage compartment.

The prepared project did not receive any further development, the GVF in this class of vehicles was quite satisfied with the Il-12 and Il-14 piston engines.

MAIN DATA TU-111
Take-off weight, kg 20 000
Full load, kg 2160
Maximum speed altitude of 5000-8000 m, km / h 700
Practical ceiling, m 10 300
Range of flight, km 2200
Number of passengers 24 people
Crew, people 3
Length m 21,8
Wingspan m 21.9
Wing area, m2 60,0




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Page last modified: 14-12-2017 17:05:13 ZULU