About: Westinghouse J30   Sponge Permalink

An Entity of Type : dbkwik:resource/t0EYzM3e0H-TCd0voM-X1Q==, within Data Space : 134.155.108.49:8890 associated with source dataset(s)

The Westinghouse J30, initially known as the Westinghouse 19XB, was a turbojet engine developed by Westinghouse Electric Corporation. It was the first American-designed turbojet to run, and only the second axial-flow turbojet to run outside of Germany. A simple and robust unit with six-stage compressor, annular combustor, and single-stage turbine, it initially gave 1,200 pounds of thrust. Its first flight was under a FG Corsair in January 1944. It was developed into the smaller J32, and the successful Westinghouse J34, an enlarged version which produced 3,000 pounds of thrust.

AttributesValues
rdf:type
rdfs:label
  • Westinghouse J30
rdfs:comment
  • The Westinghouse J30, initially known as the Westinghouse 19XB, was a turbojet engine developed by Westinghouse Electric Corporation. It was the first American-designed turbojet to run, and only the second axial-flow turbojet to run outside of Germany. A simple and robust unit with six-stage compressor, annular combustor, and single-stage turbine, it initially gave 1,200 pounds of thrust. Its first flight was under a FG Corsair in January 1944. It was developed into the smaller J32, and the successful Westinghouse J34, an enlarged version which produced 3,000 pounds of thrust.
sameAs
combustion
  • Annular stainless steel
Developed Into
Length
  • 19(xsd:integer)
dcterms:subject
dbkwik:military/pr...iPageUsesTemplate
Type
  • Turbojet
  • Axial flow turbojet
first run
  • 1943-03-19(xsd:date)
fueltype
  • 100(xsd:integer)
major applications
Weight
  • 19(xsd:integer)
Thrust
  • at 18,000 rpm at sea level, 19B at 18,000 rpm at sea level
Manufacturer
aircon
  • /sec at 17,000 rpm, 19B /sec at 18,000 rpm
thrust/weight
  • 1(xsd:double)
National Origin
specfuelcon
  • 1(xsd:double)
oilsystem
  • pressure spray at dry sump, 60 S.U. secs grade oil
compression
  • 3(xsd:integer)
turbine
  • Single-stage axial
compressor
  • 6(xsd:integer)
abstract
  • The Westinghouse J30, initially known as the Westinghouse 19XB, was a turbojet engine developed by Westinghouse Electric Corporation. It was the first American-designed turbojet to run, and only the second axial-flow turbojet to run outside of Germany. A simple and robust unit with six-stage compressor, annular combustor, and single-stage turbine, it initially gave 1,200 pounds of thrust. Its first flight was under a FG Corsair in January 1944. It was developed into the smaller J32, and the successful Westinghouse J34, an enlarged version which produced 3,000 pounds of thrust.
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