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X-2

 

 The Bell X-2 "Starbuster" was a research aircraft built to investigate flight characteristics in the Mach 2-3 range.  Providing adequate stability and control for aircraft flying at high supersonic speeds was only one of the major difficulties facing flight researchers as they approached Mach 3. For, at speeds in that region, they knew they would also begin to encounter a "thermal barrier", severe heating effects caused by aerodynamic friction. Constructed of stainless steel and a copper-nickel alloy, and powered by a two-chamber XLR25 2,500 to 15,000 lbf (11 to 67 kN) sea level thrust throttleable rocket engine, the swept-wing Bell X-2 was designed to probe this region

 

TECHNICAL DATA

Description Specifications
Manufacturer: Bell Length: 37 ft 10 in
First Flight: 18 November 1955 Height: 11 ft 10 in
Enter Service: N/A Wing Span: 32 ft 3 in
Model:  Wing Area: 
Crew: 1 Empty Weight: 12,375 lb
Nickname: Starbuster" Max. Weight: 24,910 lb
Basic Role: Research aircraft Armament: None
Other Versions: 

Propulsion

Principal User: U. S. Airforce, National Advisory Committee for Aeronautics

Power Plant: Curtiss-Wright XLR25 rocket engine

Performance

Horsepower: 15,000 lbf at sea level
Range:  No. Of Engines: 1
Max. Speed:  Mach 3.196

Drawing

Ceiling: 126,200 ft
Climb Rate:   Photo Unknown

 


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