Specifications .28J73-GE-5.29 General Electric J73
1 specifications (j73-ge-5)
1.1 general characteristics
1.2 components
1.3 performance
specifications (j73-ge-5)
data flight.
general characteristics
type: turbojet
length: 200 in (5 m)
diameter: 39.5 in (1 m)
dry weight: 3,650 lb (1,656 kg)
components
compressor: 12 stage, axial flow, variable inlet guide vanes
combustors: 10 cannular combustion chambers
turbine: 2 stage
performance
maximum thrust: 9,500 lbf (42 kn) dry, 12,500 lbf (55.6 kn) afterburner
overall pressure ratio: 7.5:1
air mass flow: 155 lb/s (70 kg/s)
specific fuel consumption: 0.9 lb/(h lbf) (dry power)
thrust-to-weight ratio: 3.4 lbf/lb
^ flight, 9 april 1954, p.457. retrieved: 6 february 2009
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