Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
gptkb:surface-to-air_missile |
| gptkbp:developedBy |
gptkb:Nazi_Germany
gptkb:Wernher_von_Braun |
| gptkbp:diameter |
1.65 m
|
| gptkbp:engineType |
gptkb:piston_engine
|
| gptkbp:enteredService |
1944
|
| gptkbp:firstFlight |
1942
|
| gptkbp:guidanceSystem |
gyroscopic
|
| gptkbp:launched |
gptkb:Peenemünde_Army_Research_Center
|
| gptkbp:launchMass |
12,500 kg
|
| gptkbp:length |
14 m
|
| gptkbp:maximumSpeed |
5,760 km/h
|
| gptkbp:notableFor |
first human-made object to reach space
first long-range guided ballistic missile |
| gptkbp:propulsion |
ethanol
liquid oxygen |
| gptkbp:range |
320 km
|
| gptkbp:successor |
gptkb:R-1_(Soviet)
|
| gptkbp:targetedCity |
gptkb:Antwerp
gptkb:London |
| gptkbp:thrust |
25,000 lbf
|
| gptkbp:totalProduced |
over 3,000 units
|
| gptkbp:usedBy |
gptkb:German_Army
|
| gptkbp:usedDuring |
gptkb:World_War_II
|
| gptkbp:warheadType |
1,000 kg Amatol
|
| gptkbp:bfsParent |
gptkb:Aggregat_rocket_series
|
| gptkbp:bfsLayer |
5
|
| https://www.w3.org/2000/01/rdf-schema#label |
A-4 (V-2 rocket)
|