Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:combustionChambers |
1
15 bar |
| gptkbp:coolingSystem |
regenerative cooling
|
| gptkbp:countryOfOrigin |
gptkb:Germany
|
| gptkbp:designer |
gptkb:Wernher_von_Braun
|
| gptkbp:developedBy |
gptkb:Nazi_Germany
gptkb:Peenemünde_Army_Research_Center |
| gptkbp:firstFlight |
1942
|
| gptkbp:fuelType |
ethanol
|
| https://www.w3.org/2000/01/rdf-schema#label |
German V-2 engine
|
| gptkbp:influenced |
early US and Soviet rocket programs
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
liquid-fueled
|
| gptkbp:thrust |
25 metric tons
|
| gptkbp:usedBy |
gptkb:Wehrmacht
|
| gptkbp:usedDuring |
gptkb:World_War_II
|
| gptkbp:usedFor |
ballistic missile propulsion
|
| gptkbp:usedIn |
gptkb:V-2_rocket
|
| gptkbp:bfsParent |
gptkb:RD-20
|
| gptkbp:bfsLayer |
7
|