|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:associated_with
|
gptkb:paper
|
|
gptkbp:average_temperature
|
1,000 ° C
|
|
gptkbp:check_in_time
|
60 seconds
|
|
gptkbp:conflict
|
gptkb:World_War_II
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:debut
|
October 3, 1944
|
|
gptkbp:decommissioned
|
1945
|
|
gptkbp:designed_by
|
gptkb:Wernher_von_Braun
|
|
gptkbp:development
|
gptkb:Nazi_Germany
|
|
gptkbp:diameter
|
1.65 meters
|
|
gptkbp:engine
|
gas-generator cycle
|
|
gptkbp:engine_configuration
|
single-chamber
|
|
gptkbp:exhaust_system
|
converging-diverging nozzle
|
|
gptkbp:first_flight
|
gptkb:1944
1943
|
|
gptkbp:fuel_economy
|
0.5 kg per second
|
|
gptkbp:fuel_tank_material
|
aluminum
|
|
gptkbp:fuel_type
|
liquid oxygen and alcohol
|
|
gptkbp:guidance_system
|
gyroscopic guidance
|
|
gptkbp:has_research_center
|
gptkb:Peenemünde_Army_Research_Center
|
|
gptkbp:historical_impact
|
pioneered ballistic missile technology
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
German V-2 rocket engine
|
|
gptkbp:ignition_system
|
hypergolic ignition
|
|
gptkbp:influenced
|
gptkb:space_exploration
|
|
gptkbp:inspired
|
gptkb:NASA's_Saturn_V
|
|
gptkbp:inspired_development
|
ICBM technology
|
|
gptkbp:investment
|
6.5 bar
|
|
gptkbp:is_influenced_by
|
modern rocketry
|
|
gptkbp:launch_mass
|
12,000 kg
|
|
gptkbp:launch_site
|
gptkb:Peenemünde
|
|
gptkbp:legacy
|
foundation for future space missions
|
|
gptkbp:length
|
4.88 meters
|
|
gptkbp:military_technology
|
strategic bombing
|
|
gptkbp:notable_feature
|
high speed
high altitude capability
first operational ballistic missile
guided trajectory
|
|
gptkbp:number_of_rooms
|
cylindrical
|
|
gptkbp:operated_by
|
gptkb:Wehrmacht
|
|
gptkbp:operational_range
|
320 km
|
|
gptkbp:operational_use
|
March 1945
|
|
gptkbp:oxidizer_tank_material
|
gptkb:steel
|
|
gptkbp:post_war_career
|
Cold War missile development
|
|
gptkbp:price
|
100,000 Reichsmarks
|
|
gptkbp:propulsion
|
25,000 pounds
Ethanol and liquid oxygen
|
|
gptkbp:related_to
|
gptkb:A-4_rocket
|
|
gptkbp:significance
|
first long-range guided ballistic missile
|
|
gptkbp:successor
|
gptkb:Redstone_rocket
|
|
gptkbp:technology
|
gptkb:Team_Rocket
|
|
gptkbp:used_by
|
gptkb:Nazi_Germany
|
|
gptkbp:used_in
|
gptkb:V-2_rocket
|
|
gptkbp:weight
|
3,000 kg
|
|
gptkbp:bfsParent
|
gptkb:RD-500_rocket_engine
|
|
gptkbp:bfsLayer
|
7
|