Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:Heinkel_He_178
|
| gptkbp:aircraft_operated |
gptkb:Heinkel_He_162
gptkb:Messerschmitt_Me_262 |
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:date |
1939
|
| gptkbp:diameter |
0.9 m
|
| gptkbp:engine |
turbojet
|
| gptkbp:engine_type |
axial
single-stage |
| gptkbp:first_flight |
1941
|
| gptkbp:fuel_type |
kerosene
annular combustion chamber |
| https://www.w3.org/2000/01/rdf-schema#label |
Heinkel He S 3
|
| gptkbp:length |
3.2 m
|
| gptkbp:manufacturer |
Heinkel
|
| gptkbp:power_output |
1,000 lbf
|
| gptkbp:produced_by |
retired
|
| gptkbp:propulsion |
5.0
|
| gptkbp:successor |
gptkb:Heinkel_He_S_011
|
| gptkbp:type |
gptkb:engine
|
| gptkbp:used_in |
gptkb:Heinkel_He_280
|
| gptkbp:weight |
200 kg
|