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The XB-70A, built by North American Aviation's Los Angeles (Calif.) Division for the U.S. Air Force, was an experimental high-speed, delta-wing aircraft designed to fly at three times the speed of sound and at altitudes in excess of 70,000 feet.
It was powered by six General Electric J-93 turbojet engines, each producing approximately 30,000 pounds of thrust. Primary purpose of the aircraft was to investigate the feasibility of long-range, high-speed flight and to advance the aeronautical state of the art in those areas.
Among its design features were a movable canard, the "compression lift" aerodynamic design principle, in-flight accessibility to electronics equipment, a shirt-sleeve environment for the crew, and encapsulated seats for crew ejection at speeds up to Mach 3 and at altitudes to above 70,000 feet.
A rugged landing gear, weighing more than six tons and consisting of two tons of wheels, tires and brakes, supported the XB-70 on the ground. Each main gear had four wheels and the nose gear two. In a single stop, the XB-70 absorbed kinetic energy equivalent to that used in stopping 800 medium-size automobiles from a speed of about 100 miles an hour.
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Unique identifier
BI45090
Boeing ID
BIV15_XB-70_01
Type
Video
Duration
3m59s
Size
720px × 480px 84MB
License type
RM
Keywords
1960s
airplanes
bombers
clear skies
day
deserts
exteriors
flying
flying in formation
full body views
futuristic
ground shots
historic production status
jets
landing gears
military
military livery
monoplanes
nobody
parachutes, parafoils and drag chutes
prototypes
runways
smoke
sunshine
test flights
white