Bell X-2

E17995

The Bell X-2 was a rocket-powered experimental research aircraft developed in the 1950s to investigate flight characteristics at extremely high speeds and altitudes, contributing crucial data to early supersonic and space-era aeronautics.


Statements (49)
Predicate Object
instanceOf X-plane
experimental aircraft
research aircraft
rocket-powered aircraft
accident fatal crash on 1956-09-27
carrierAircraft B-50 Superfortress
constructionMaterial K-monel
stainless steel
countryOfOrigin United States
crashCause loss of control due to inertial coupling
crew 1
engineType liquid-fueled rocket engine
fatalities 1 in 1956 crash
firstFlight 1952-11-18
firstPoweredFlight 1955-11-18
fuselageType slender streamlined fuselage
introduced 1955
landingGear retractable tricycle landing gear
launchMethod air launch from carrier aircraft
manufacturer Bell Aircraft
maximumAltitude over 126,000 feet
over 38,000 meters
maximumSpeed about Mach 3.2
approximately 3,370 km/h
notableFlight record Mach 3.2 flight by Milburn G. Apt
numberBuilt 2
operator National Advisory Committee for Aeronautics
United States Air Force
powerplant Curtiss-Wright XLR25 rocket engine
primaryUser United States Air Force
program X-plane program
purpose high-altitude research
high-speed research
investigation of flight characteristics at Mach 2–3
study of aerodynamic heating
study of stability and control at very high Mach numbers
record first aircraft to exceed Mach 3 in level flight
researchContribution contributed to design of later high-speed aircraft
data on aerodynamic heating at Mach 2–3
data on stability and control at very high Mach numbers
informed early space-era aeronautics
retired 1956
status retired
successorInRole Bell X-15
tailConfiguration conventional tail unit
testPilot Frank K. Everest Jr.
Iven C. Kincheloe Jr.
Milburn G. Apt
wingConfiguration mid-wing monoplane

Referenced by (2)

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