gptkbp:instanceOf
|
rocket
|
gptkbp:controls
|
gyroscopic_control
|
gptkbp:decommissioned
|
1950
|
gptkbp:deployedTo
|
gptkb:U.S._military
|
gptkbp:design
|
gptkb:Nazi_Germany
|
gptkbp:developer
|
gptkb:United_States
gptkb:World_War_II
|
gptkbp:diameter
|
1.65 meters
|
gptkbp:engine
|
liquid-fueled
|
gptkbp:engineType
|
liquid rocket engine
|
gptkbp:firstFlight
|
1944
successful
|
gptkbp:firstGeneration
|
none
|
gptkbp:fuelType
|
kerosene and liquid oxygen
|
gptkbp:gameFeatures
|
RP-1 and LOX
|
gptkbp:hasArea
|
320 km
|
gptkbp:historicalSignificance
|
pioneered missile technology
|
https://www.w3.org/2000/01/rdf-schema#label
|
US 7,000,000 V2
|
gptkbp:influenced
|
V-2 rocket
future missile designs
|
gptkbp:influencedBy
|
gptkb:Germany
gptkb:V-2_program
V-2 rocket
German_rocket_technology
|
gptkbp:inspiredBy
|
V-2 rocket technology
|
gptkbp:launched
|
vertical launch
|
gptkbp:launchSite
|
gptkb:Peenemünde
mobile launcher
mobile launch system
|
gptkbp:legacy
|
foundation_for_modern_ICBMs
|
gptkbp:length
|
14.3 meters
|
gptkbp:manufacturer
|
gptkb:United_States
|
gptkbp:maxTakeoffWeight
|
12,500 kg
|
gptkbp:militaryRank
|
gptkb:U.S._Army
none
|
gptkbp:notableFeature
|
first long-range guided ballistic missile
|
gptkbp:notableUsers
|
gptkb:U.S._Army
|
gptkbp:numberBuilt
|
over 3,000
|
gptkbp:operationalArea
|
none
|
gptkbp:operationalStatus
|
1944-1950
|
gptkbp:origin
|
gptkb:Germany
|
gptkbp:payloadCapacity
|
1,000 kg
|
gptkbp:productionCompany
|
1940s
|
gptkbp:provides
|
1,500 meters
inertial navigation
|
gptkbp:range
|
320 km
|
gptkbp:retired
|
1950s
|
gptkbp:retirementYear
|
advancements in missile technology
|
gptkbp:status
|
retired
|
gptkbp:successor
|
gptkb:Atlas_missile
LGM-30 Minuteman
|
gptkbp:supportRole
|
none
|
gptkbp:team
|
gptkb:Wernher_von_Braun
|
gptkbp:technology
|
gptkb:intercontinental_ballistic_missile
|
gptkbp:type
|
nuclear
ballistic missile
|
gptkbp:usedBy
|
gptkb:United_States_Army
|
gptkbp:weight
|
12,500 kg
|