Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
6
|
| gptkbp:bfsParent |
gptkb:Heinkel_aircraft
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:date |
1940s
|
| gptkbp:developer |
gptkb:World_War_II
|
| gptkbp:diameter |
0.9 m
|
| gptkbp:engine |
turbojet
|
| gptkbp:engine_type |
axial compressor
single-stage turbine |
| gptkbp:fuel_type |
kerosene
annular combustion chamber |
| https://www.w3.org/2000/01/rdf-schema#label |
Heinkel He S 021
|
| gptkbp:length |
3.2 m
|
| gptkbp:manufacturer |
Heinkel
|
| gptkbp:notable_for |
gptkb:Heinkel_He_162
|
| gptkbp:operational_area |
1945
|
| gptkbp:origin |
gptkb:government_agency
|
| gptkbp:original_run |
gptkb:1944
|
| gptkbp:propulsion |
1,800 lbf
|
| gptkbp:successor |
gptkb:Heinkel_He_S_011
|
| gptkbp:type |
gptkb:engine
|
| gptkbp:weight |
1,200 lb
|