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gptkbp:instanceOf
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rocket technology
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|
gptkbp:capturedBy
|
gptkb:Soviet_Union
gptkb:United_States
|
|
gptkbp:demonstrates
|
supersonic flight
controlled reentry
vertical launch
|
|
gptkbp:developedBy
|
gptkb:Nazi_Germany
|
|
gptkbp:diameter
|
1.65 meters
|
|
gptkbp:engineType
|
liquid-propellant rocket engine
|
|
gptkbp:fuelType
|
ethanol
|
|
gptkbp:guidanceSystem
|
gyroscopic guidance
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
V-2 rocket technology
|
|
gptkbp:influenced
|
gptkb:Soviet_missile_program
US missile program
|
|
gptkbp:introducedIn
|
1944
|
|
gptkbp:keyEngineer
|
gptkb:Wernher_von_Braun
|
|
gptkbp:launched
|
mobile launch platform
|
|
gptkbp:ledTo
|
gptkb:R-1_rocket
gptkb:Redstone_rocket
|
|
gptkbp:length
|
14 meters
|
|
gptkbp:mass
|
12,500 kg
|
|
gptkbp:oxidizer
|
liquid oxygen
|
|
gptkbp:payload
|
explosive warhead
|
|
gptkbp:propulsion
|
liquid-fueled
|
|
gptkbp:range
|
320 km
|
|
gptkbp:target
|
gptkb:Antwerp
gptkb:London
|
|
gptkbp:thrust
|
25 metric tons
|
|
gptkbp:usedDuring
|
gptkb:World_War_II
|
|
gptkbp:usedFor
|
gptkb:surface-to-air_missile
|
|
gptkbp:usedIn
|
gptkb:V-2_rocket
|
|
gptkbp:bfsParent
|
gptkb:Hermes_missile_program
|
|
gptkbp:bfsLayer
|
7
|