编辑“︁Jumo 004”︁（章节）

==主要性能參數 (Jumo 004B)==
[[File:JUMO 004 Jet Propelled Engine GPN-2000-000369.jpg|thumb|A Jumo 004 engine is being investigated by Aircraft Engine Research Laboratory engineers of the [[National Advisory Committee for Aeronautics]] in 1946]]
{{jetspecs
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|ref={{citation needed|date=June 2012}}
|type=[[渦輪噴射發動機|渦輪噴射]]
|length=3.86 m (152 in)
|diameter=81 cm (32 in)
|weight=719 kg (1,585 lb)
|compressor=8-級 [[压气机|軸流式壓縮機]]
|combustion=Can-type, 6
|turbine=Single-stage
|fueltype=
|oilsystem=
|power=
|thrust=8.8 kN (1,980 lbf) at 8,700 rpm
|compression=3.14:1
|fuelcon=
|specfuelcon=1.39 N/(N·hr)
|power/weight=
|thrust/weight=1.25 (12.2 N/kg)
}}