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Tupolev Tu-360

Military Aircraft

The Tupolev Tu-360 was a proposed hypersonic strategic bomber conceived by the Tupolev design bureau in the 1980s, using most of the same technologies as the Tu-2000. The bureau intended it as a potential replacement for the Tu-160, with the same layout as the Mach 4 Tu-230 but much larger and faster. Speeds around Mach 6 required liquid hydrogen fuel, and the engines used the same liquid hydrogen ramjet technology as the Tu-2000. Weapons were to sit in two bomb bays, take-off weight was projected near 350,000 kg and the weapons load at 10,000 kg. A subscale technology demonstrator of 80,000 kg was planned, but a lack of funds after the fall of the Soviet Union meant the project was axed in 1992.

Facts
Propulsion
Hydrogen 1
Engine Class
Ramjet 1
Status
Cancelled 1
Maximum Mass (kg)
350,000 1
Comparison
Body Style
Aircraft (no road body style) 1
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Aviation, Modes
Source Tupolev Tu-360 (Wikipedia)

Of Make

Source Tupolev Tu-360 (Wikipedia)
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Source Tupolev Tu-360 (Wikipedia)Lead
Quote, Lead
was a proposed hypersonic strategic bomber conceived by the Tupolev design bureau
Sources
1. Tupolev Tu-360 (Wikipedia)
  • Lead
    was a proposed hypersonic strategic bomber conceived by the Tupolev design bureau
  • Design and development
    the project was axed in 1992
  • Design and development, engine class
    liquid hydrogen ramjet engine technology
  • Design and development, propulsion
    Speeds at Mach 6 required the use of liquid hydrogen
  • Specifications
    Max takeoff weight: 350,000 kg (771,618 lb)
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