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Tupolev '102'

Airliners and Commercial Jet Aircraft

The Tupolev '102' was a 1950s project by the Tupolev Design Bureau for a turboprop airliner, drawn up alongside the almost identical Tupolev '101' assault transport. The '102' had a pressurised cabin in one section, configured for 40 passengers, where the '101' had a rear loading ramp, a tail barbette for two Nudelman-Rikhter NR-23 cannon and an unpressurised cabin apart from the flightdeck and a small cabin for ten passengers. Both were projected with two Kuznetsov TV-2F turboprop engines of 5,200 kW each, a wingspan of 40 m, a gross weight of 36,000 kg and a top speed of 650 to 700 km/h. Similar requirements were issued to the Myasishchev and Antonov bureaus, and the Antonov response became the An-8, which formed the design root of all Antonov turboprop transports up to the An-22. The Tupolev designs were not built.

Facts
Engine Class
Turboprop 1
Status
Design only (never built) 1
Comparison
Body Style
Aircraft (no road body style) 1
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Exemplifies

Aviation, Modes
Source Tupolev '102' (Wikipedia)

Of Make

Source Tupolev '102' (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Tupolev '102' (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
by the Tupolev Design Bureau
Sources
1. Tupolev '102' (Wikipedia)
  • Lead
    were 1950s projects for a turboprop airliner and assault transport by the Tupolev Design Bureau
  • Lead, status
    were 1950s projects for a turboprop airliner and assault transport
  • Specifications
    2 × Kuznetsov TV-2F turboprop engines
  • Lead, manufacturer
    by the Tupolev Design Bureau
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