|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:advances
|
guided missile technology
|
|
gptkbp:associated_with
|
gptkb:Third_Reich
gptkb:paper
gptkb:Nazi_rocket_scientists
|
|
gptkbp:debut
|
October 3, 1944
|
|
gptkbp:decommissioned
|
1945
|
|
gptkbp:designed_by
|
gptkb:Wernher_von_Braun
|
|
gptkbp:developed_by
|
gptkb:Germany
|
|
gptkbp:development
|
1930s to 1945
|
|
gptkbp:fighting_style
|
September 1944
against Allied cities
|
|
gptkbp:first_flight
|
gptkb:1944
October 1944
|
|
gptkbp:fuel_type
|
liquid oxygen and alcohol
|
|
gptkbp:guidance_system
|
inertial guidance
|
|
gptkbp:historical_context
|
World War II technology
|
|
gptkbp:historical_impact
|
shaped future of warfare
|
|
gptkbp:historical_significance
|
first long-range guided ballistic missile
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
V-2 rocket program
|
|
gptkbp:impact
|
gptkb:space_exploration
|
|
gptkbp:influenced
|
gptkb:Soviet_space_program
aerospace engineering
modern military strategy
missile defense systems
post-war rocketry
|
|
gptkbp:influenced_by
|
gptkb:A-4_rocket
gptkb:V-1_flying_bomb
German rocket research
V-2 test flights
|
|
gptkbp:inspired
|
gptkb:space_exploration
gptkb:NASA's_Apollo_program
|
|
gptkbp:inspired_technologies
|
satellite launch vehicles
|
|
gptkbp:involved
|
German engineers
|
|
gptkbp:involved_in
|
rocket science advancements
space race developments
|
|
gptkbp:is_driven_by
|
ethanol and liquid oxygen
|
|
gptkbp:is_targeted_at
|
gptkb:London
|
|
gptkbp:key_figures
|
gptkb:Wernher_von_Braun
|
|
gptkbp:launch_site
|
gptkb:Peenemünde
|
|
gptkbp:launch_vehicle
|
gptkb:A-4
|
|
gptkbp:launched
|
3,000
over 3,000
90 degrees
over 1,400
|
|
gptkbp:legacy
|
gptkb:space_exploration
modern rocketry
|
|
gptkbp:length
|
14 meters
|
|
gptkbp:location
|
gptkb:Peenemünde_Army_Research_Center
|
|
gptkbp:manufacturer
|
gptkb:Dornier
|
|
gptkbp:military_technology
|
military research
|
|
gptkbp:notable_feature
|
vertical launch
first long-range guided ballistic missile
|
|
gptkbp:operated_by
|
gptkb:Nazi_Germany
|
|
gptkbp:operational_period
|
1944-1945
|
|
gptkbp:operational_use
|
gptkb:1944
|
|
gptkbp:original_purpose
|
gptkb:weapons
|
|
gptkbp:payload_capacity
|
1,000 kg
|
|
gptkbp:post_war_career
|
Cold War arms race
|
|
gptkbp:primary_user
|
gptkb:Nazi_Germany
|
|
gptkbp:production_years
|
1943
1945
|
|
gptkbp:range
|
320 km
|
|
gptkbp:research
|
aerodynamics
|
|
gptkbp:speed
|
5,760 km/h
|
|
gptkbp:success_rate
|
approximately 50%
|
|
gptkbp:successor
|
gptkb:A-4_rocket
gptkb:Redstone_rocket
|
|
gptkbp:technology
|
liquid-fueled rocket engine
|
|
gptkbp:type
|
gptkb:missile
|
|
gptkbp:used_by
|
German military
|
|
gptkbp:used_in
|
gptkb:World_War_II
|
|
gptkbp:warhead_type
|
high explosive
|
|
gptkbp:weight
|
13,000 kg
|
|
gptkbp:bfsParent
|
gptkb:Hermann_Oberth
|
|
gptkbp:bfsLayer
|
4
|