About: Bristol Siddeley BS100   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 Bristol Siddeley BS.100 was a British twin-spool, vectored thrust, turbofan aero engine that first ran in 1960, the engine was designed and built in limited numbers by Bristol Siddeley Engines Limited. The project was cancelled in early 1965.

AttributesValues
rdf:type
rdfs:label
  • Bristol Siddeley BS100
rdfs:comment
  • The Bristol Siddeley BS.100 was a British twin-spool, vectored thrust, turbofan aero engine that first ran in 1960, the engine was designed and built in limited numbers by Bristol Siddeley Engines Limited. The project was cancelled in early 1965.
sameAs
combustion
  • annular
dcterms:subject
dbkwik:military/pr...iPageUsesTemplate
Type
  • Turbofan
  • Vectored thrust turbofan
major applications
Thrust
  • * PCB off * short lift thrust, PCB on
Manufacturer
aircon
  • /sec
thrust/weight
  • :1
specfuelcon
  • *0.615 lb/ at dry thrust *1.16 lb/ with PCB
compression
  • 11(xsd:double)
Number Built
  • 6(xsd:integer)
compressor
  • Two-spool axial flow Bypass ratio: 0.9:1
abstract
  • The Bristol Siddeley BS.100 was a British twin-spool, vectored thrust, turbofan aero engine that first ran in 1960, the engine was designed and built in limited numbers by Bristol Siddeley Engines Limited. The project was cancelled in early 1965.
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