Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:combustionChambers |
15 bar
|
| gptkbp:countryOfOrigin |
gptkb:Germany
|
| gptkbp:cycle |
gas-generator cycle
|
| gptkbp:developedBy |
gptkb:Nazi_Germany
gptkb:Wernher_von_Braun |
| gptkbp:diameter |
0.8 m
|
| gptkbp:firstFlight |
1942
|
| gptkbp:fuelType |
ethanol
|
| gptkbp:influenced |
gptkb:American_Redstone_rocket_engine
gptkb:Soviet_R-1_rocket_engine |
| gptkbp:length |
1.6 m
|
| gptkbp:numberOfRooms |
1
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
ethanol
liquid oxygen |
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:Redstone_rocket_engine
|
| gptkbp:thrust |
25 metric tons
245 kN |
| gptkbp:usedDuring |
gptkb:World_War_II
|
| gptkbp:usedFor |
gptkb:surface-to-air_missile
|
| gptkbp:usedIn |
gptkb:V-2_rocket
|
| gptkbp:bfsParent |
gptkb:New_Mexico_Museum_of_Space_History
|
| gptkbp:bfsLayer |
5
|
| https://www.w3.org/2000/01/rdf-schema#label |
V-2 rocket engine
|