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The Pilots Desk
Airlinerssupersonic airliner design by Boeing

Boeing 2707

Boeing 2707

The Boeing 2707 was an American supersonic passenger airliner project during the 1960s. After winning a competition for a government-funded contract to build an American supersonic airliner, Boeing began development at its facilities in Seattle, Washington. The design emerged as a large aircraft with seating for 250 to 300 passengers and cruise speeds of approximately Mach 3. It was intended to be much larger and faster than competing supersonic transport (SST) designs such as the Concorde. The SST was the topic of considerable concern within and outside the aviation industry. From the start, the airline industry noted that the economics of the design were questionable, concerns that were only partially addressed during development. Outside the field, the entire SST concept was the subject of considerable negative press, centered on the issue of sonic booms and effects on the ozone layer. A key design feature of the 2707 was its use of a swing-wing configuration. During development, the required weight and size of this mechanism continued to grow, forcing the team to switch to a conventional delta wing. Rising costs, environmental concerns, noise, and the lack of a clear market led to its cancellation in 1971 before two prototypes were completed.

Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.

Category
Airliners
Country of origin
United States
Length
93.2 m

Specifications

Cruise speed
3 kt
Max speed
3 kt
Range
2,400 nm
Service ceiling
65,000 ft
Rate of climb
4,000 ft/min
Max takeoff weight
550,000 lb
Empty weight
300,000 lb
Fuel capacity
24,000 US gal
Powerplant
General Electric GE4/J5
Engines
4
Seats
300
Length
275 ft
Wingspan
200 ft
Height
40 ft

Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).

Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.