|
gptkbp:instanceOf
|
rocket
|
|
gptkbp:airlines
|
100 km
15 minutes
|
|
gptkbp:associatedWith
|
gptkb:Cold_War
|
|
gptkbp:chemicalFormula
|
liquid oxygen
|
|
gptkbp:controls
|
gyroscopic_control
|
|
gptkbp:decommissioned
|
1945
|
|
gptkbp:design
|
1940s
aerodynamic shape
|
|
gptkbp:designedBy
|
gptkb:Wernher_von_Braun
|
|
gptkbp:developer
|
1945
German_engineers
|
|
gptkbp:diameter
|
1.2 meters
|
|
gptkbp:engine
|
100 kN
|
|
gptkbp:engineConfiguration
|
single engine
|
|
gptkbp:engineType
|
liquid-fueled engine
|
|
gptkbp:firstFlight
|
1944
multiple
successful
|
|
gptkbp:fuelCapacity
|
3,000 liters
4,000 liters
|
|
gptkbp:fuelType
|
RP-1
|
|
gptkbp:gameFeatures
|
liquid oxygen and kerosene
|
|
gptkbp:hasArea
|
gptkb:Peenemünde
|
|
gptkbp:historicalContext
|
Nazi_Germany's_military_efforts
|
|
gptkbp:historicalSignificance
|
early missile technology
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
A-9 rocket
|
|
gptkbp:influencedBy
|
V-2 rocket
|
|
gptkbp:inspiration
|
World_War_II_technology
|
|
gptkbp:launched
|
45 degrees
limited
manual control
|
|
gptkbp:launchSite
|
gptkb:Peenemünde_Army_Research_Center
10,000 kg
ground launch
|
|
gptkbp:legacy
|
influenced modern rocketry
|
|
gptkbp:length
|
14.5 meters
|
|
gptkbp:manufacturer
|
gptkb:German_Aerospace_Center
|
|
gptkbp:militaryRank
|
strategic weapon
|
|
gptkbp:operationalRange
|
1,500 km
|
|
gptkbp:operationalStatus
|
1944-1945
|
|
gptkbp:payloadCapacity
|
1,000 kg
|
|
gptkbp:postWarCareer
|
influenced space race.
|
|
gptkbp:productionCompany
|
1942
|
|
gptkbp:provides
|
inertial navigation
inertial guidance
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:relatedTo
|
gptkb:A-4_rocket
|
|
gptkbp:researchInterest
|
military research
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
A-10 rocket
|
|
gptkbp:targets
|
military installations
|
|
gptkbp:technology
|
classified
|
|
gptkbp:type
|
nuclear
ballistic missile
|
|
gptkbp:usedBy
|
gptkb:Nazi_Germany
|
|
gptkbp:weight
|
10,000 kg
|