PropertyValue
rdf:type
rdfs:label
  • Bell X-2
rdfs:comment
  • The Bell X-2 (nicknamed "Starbuster") was a research aircraft built to investigate flight characteristics in the Mach 2–3 range. The X-2 was a rocket-powered, swept-wing research aircraft developed jointly in 1945 by Bell Aircraft Corporation, the U.S. Air Force and the National Advisory Committee for Aeronautics (NACA) to explore aerodynamic problems of supersonic flight and to expand the speed and altitude regimes obtained with the earlier X-1 series of research aircraft.
owl:sameAs
dcterms:subject
dbkwik:military/property/wikiPageUsesTemplate
max takeoff weight alt
  • 11300.0
loaded weight main
  • 24910.0
airfoil
  • 2
length alt
  • 11.5 m
span main
  • 982.98
thrust alt
  • 67 kN
height alt
  • 3.6 m
primary user
Type
  • Research aircraft
length main
  • 1153.16
area main
  • 260.0
height main
  • 360.68
span alt
  • 9.8 m
Manufacturer
  • Bell Aircraft
max speed main
  • Mach 3.196
ceiling main
  • 126200.0
National Origin
empty weight main
  • 12375.0
type of jet
loaded weight alt
  • 11300.0
thrust original
  • at sea level
area alt
  • 24.2
First Flight
  • 1955-11-18
more users
engine (jet)
  • Curtiss-Wright XLR25
max speed alt
  • 2094
jet or prop?
  • jet
empty weight alt
  • 5600.0
thrust main
  • 15000
number of jets
  • 1
plane or copter?
  • plane
ceiling alt
  • 38,466 m
max takeoff weight main
  • 24910.0
Retired
  • 1956-09-27
Crew
  • one, pilot
Number Built
  • 2
ref
  • Concept Aircraft: Prototypes, X-Planes and Experimental Aircraft
abstract
  • The Bell X-2 (nicknamed "Starbuster") was a research aircraft built to investigate flight characteristics in the Mach 2–3 range. The X-2 was a rocket-powered, swept-wing research aircraft developed jointly in 1945 by Bell Aircraft Corporation, the U.S. Air Force and the National Advisory Committee for Aeronautics (NACA) to explore aerodynamic problems of supersonic flight and to expand the speed and altitude regimes obtained with the earlier X-1 series of research aircraft.