. "None"@en . "6060.0"^^ . . "to at"@en . . . . "to"@en . "*Take-off run: \n*Landing run '102': \n**Landing run '101': with reverse pitch"@en . "met"@en . . . "40"^^ . "OKB Tupolev : a history of the design bureau and its aircraft"@en . . . "3851"^^ . . "40"^^ . . . . "6060.0"^^ . "6060.0"^^ . "650"^^ . . . "6060.0"^^ . "The Tupolev '102' and Tupolev '101' were 1950s projects for a turboprop airliner and assault transport by the Tupolev Design Bureau. The aircraft designs were almost identical but the '101' had a rear loading ramp and tail barbette for two Nudelman-Rikhter NR-23 cannon. The internal arrangement also differed with the '101' cabin being unpressurised apart from the flightdeck and a small cabin for ten passengers, whilst the '102's pressurised cabin was in one section, configured for 40 passengers."@en . . . . . "1000"^^ . . . "The Tupolev '102' and Tupolev '101' were 1950s projects for a turboprop airliner and assault transport by the Tupolev Design Bureau. The aircraft designs were almost identical but the '101' had a rear loading ramp and tail barbette for two Nudelman-Rikhter NR-23 cannon. The internal arrangement also differed with the '101' cabin being unpressurised apart from the flightdeck and a small cabin for ten passengers, whilst the '102's pressurised cabin was in one section, configured for 40 passengers. Similar requirements were also issued to OKB-23 (V.M. Myasischchev) and (Oleg K. Antonov), resulting in the Antonov An-8 which formed the design root of all Antonov's turboprop transports up to the An-22."@en . . . . "7000"^^ . . . . . "Tupolev '102'"@en . . "3.8"^^ . . ""@en . "-"@en . . . . "36000"^^ . . "6060.0"^^ . "fuselage"@en . "turboprop engines"@en . "1087304075"^^ . "40"^^ . . . "20206227"^^ . . "140"^^ . "2"^^ . . . . . . . "/"@en . "7"^^ . "6070.0"^^ . . . "3000"^^ .