Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:combustionChambers |
1
15 bar |
| gptkbp:countryOfOrigin |
gptkb:Germany
|
| gptkbp:developedBy |
gptkb:Nazi_Germany
gptkb:Wernher_von_Braun |
| gptkbp:diameter |
1.65 m
|
| gptkbp:engineCycle |
gas-generator cycle
|
| gptkbp:firstFlight |
1942
|
| gptkbp:length |
5.5 m
|
| gptkbp:propulsion |
ethanol
liquid oxygen |
| gptkbp:status |
retired
|
| gptkbp:thrust |
25 metric tons
245 kN |
| gptkbp:usedDuring |
gptkb:World_War_II
|
| gptkbp:usedFor |
gptkb:surface-to-air_missile
spaceflight research |
| gptkbp:usedIn |
gptkb:V-2_rocket
|
| gptkbp:bfsParent |
gptkb:Soviet_R-1_rocket_engine
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
German V-2 rocket engine
|