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gptkbp:instance_of
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gptkb:engine
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gptkbp:bfsLayer
|
6
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gptkbp:bfsParent
|
gptkb:Heinkel_He_S_3
gptkb:Heinkel_aircraft
|
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gptkbp:aircraft_operated
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gptkb:aircraft
gptkb:Heinkel_He_219
gptkb:Messerschmitt_Me_262
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gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
1,000 ° C
|
|
gptkbp:controls
|
mechanical
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|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
gptkb:Walter_Richard_Dornberger
high performance
|
|
gptkbp:developer
|
gptkb:World_War_II
1942-1944
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissions_standard
|
subsonic
straight-through
|
|
gptkbp:engine
|
gptkb:BMW_003
Brayton cycle
single-spool
|
|
gptkbp:engine_type
|
2
8
|
|
gptkbp:first_flight
|
gptkb:1944
|
|
gptkbp:fuel_capacity
|
0.8 kg/k N·h
|
|
gptkbp:fuel_type
|
kerosene
annular combustion chamber
pressure-fed
|
|
gptkbp:historical_significance
|
early turbojet technology
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Heinkel He S 011
|
|
gptkbp:ignition_system
|
gptkb:park
|
|
gptkbp:influence
|
post-war jet engine development
|
|
gptkbp:invention
|
gptkb:3
engine design patent
|
|
gptkbp:legacy
|
influenced future designs
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
100 hours
|
|
gptkbp:manufacturer
|
Heinkel
|
|
gptkbp:notable_feature
|
high thrust-to-weight ratio
|
|
gptkbp:operational_area
|
limited
|
|
gptkbp:operational_history
|
short-lived
|
|
gptkbp:produced_by
|
not mass-produced
|
|
gptkbp:propulsion
|
2,500 lbf
|
|
gptkbp:successor
|
He S 011 A
|
|
gptkbp:type
|
axial-flow turbojet
|
|
gptkbp:used_in
|
gptkb:Heinkel_He_280
|
|
gptkbp:weight
|
1,200 lb
|