About: Wright J65   Sponge Permalink

An Entity of Type : dbkwik:resource/t0EYzM3e0H-TCd0voM-X1Q==, within Data Space : dbkwik.org associated with source dataset(s)

The Wright J65 was an axial-flow turbojet engine produced by Curtiss-Wright under license from Armstrong Siddeley. A development of the Sapphire, the J65 powered a number of US designs.

AttributesValues
rdf:type
rdfs:label
  • Wright J65
rdfs:comment
  • The Wright J65 was an axial-flow turbojet engine produced by Curtiss-Wright under license from Armstrong Siddeley. A development of the Sapphire, the J65 powered a number of US designs.
sameAs
combustion
  • annular
Length
  • 122.0
  • ~122in
dcterms:subject
dbkwik:military/pr...iPageUsesTemplate
diameter
  • 37.52
Type
  • Turbojet
first run
  • 1948-10-01(xsd:date)
major applications
  • A-4 Skyhawk
  • Martin B-57 Canberra
  • Republic F-84F Thunderstreak
Weight
  • 2743.0
  • 2776.0
turbinetemp
  • ~848C
Thrust
  • 7239(xsd:integer)
Manufacturer
  • Curtiss-Wright
aircon
  • 119(xsd:double)
thrust/weight
  • 2(xsd:double)
Developed From
specfuelcon
  • ~0.916lb/hr/lbf
compression
  • 7(xsd:integer)
turbine
  • 2(xsd:integer)
compressor
  • 13(xsd:integer)
abstract
  • The Wright J65 was an axial-flow turbojet engine produced by Curtiss-Wright under license from Armstrong Siddeley. A development of the Sapphire, the J65 powered a number of US designs.
is engine (jet) of
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