|
gptkbp:instanceOf
|
rocket
|
|
gptkbp:associatedWith
|
gptkb:Cold_War
|
|
gptkbp:controls
|
aerodynamic surfaces
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:crewCapacity
|
none
|
|
gptkbp:debutYear
|
1944
|
|
gptkbp:decommissioned
|
1945
|
|
gptkbp:designatedAs
|
gptkb:US_military
|
|
gptkbp:developer
|
1944
German_V-2_program
|
|
gptkbp:diameter
|
1.65 meters
|
|
gptkbp:engine
|
1
25,000 N
|
|
gptkbp:engineType
|
liquid fuel
|
|
gptkbp:firstFlight
|
1944
|
|
gptkbp:fuelType
|
ethanol
|
|
gptkbp:historicalSignificance
|
first successful military rocket
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
US 93,000,000 V2
|
|
gptkbp:influenced
|
modern rocketry
space launch systems
liquid propulsion
|
|
gptkbp:influencedBy
|
gptkb:German_V-2_rocket
|
|
gptkbp:inspiration
|
future missile technology
|
|
gptkbp:launched
|
weekly
$10,000
|
|
gptkbp:launchSite
|
gptkb:Cape_Canaveral
12,000 kg
mobile launch platform
|
|
gptkbp:launchVehicle
|
ballistic missile
|
|
gptkbp:legacy
|
foundation for future space missions
|
|
gptkbp:length
|
14.5 meters
|
|
gptkbp:manufacturer
|
NASA
|
|
gptkbp:maxSpeed
|
5,760 km/h
|
|
gptkbp:notableFeature
|
first long-range guided ballistic missile
|
|
gptkbp:operatedBy
|
gptkb:US_military
|
|
gptkbp:operationalRange
|
320 km
|
|
gptkbp:operationalStatus
|
1944-1945
retired
|
|
gptkbp:payloadCapacity
|
1,000 kg
|
|
gptkbp:productionCompany
|
1943
|
|
gptkbp:provides
|
1000 m
inertial navigation
gyroscopic
|
|
gptkbp:range
|
320 km
|
|
gptkbp:relatedTo
|
space exploration
|
|
gptkbp:retirementYear
|
1945
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
Redstone rocket
V-2 rocket
|
|
gptkbp:targets
|
1 km
|
|
gptkbp:team
|
gptkb:Wernher_von_Braun
|
|
gptkbp:type
|
high explosive
|
|
gptkbp:usedBy
|
gptkb:US_Army
|
|
gptkbp:usedIn
|
gptkb:World_War_II
|
|
gptkbp:weight
|
12,000 kg
|