|
gptkbp:instanceOf
|
rocket engine
|
|
gptkbp:brewingProcess
|
modular design
|
|
gptkbp:compatibleWith
|
guidance and control systems
|
|
gptkbp:component
|
aluminum and titanium
|
|
gptkbp:coolingSystem
|
regenerative cooling
|
|
gptkbp:design
|
satellite launch
|
|
gptkbp:developedBy
|
gptkb:Arianespace
|
|
gptkbp:environmentalImpact
|
low emissions
|
|
gptkbp:firstFlight
|
gptkb:Ariane_1
|
|
gptkbp:fuelType
|
liquid propellant
hypergolic ignition
|
|
gptkbp:future_plans
|
next-generation propulsion systems
|
|
gptkbp:hasContent
|
up to 300 seconds
|
|
gptkbp:hasDepartment
|
approximately 150 seconds
|
|
gptkbp:hasVersion
|
gptkb:Ariane_6
|
|
gptkbp:historicalSignificance
|
pioneered commercial spaceflight
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Ariane rocket engines
|
|
gptkbp:internationalCooperation
|
ESA_and_CNES
|
|
gptkbp:keyIssues
|
high performance
commercial satellite operators
|
|
gptkbp:launchDate
|
over 250 launches
|
|
gptkbp:launched
|
competitive
multiple launches per year
up to 10,000 kg to GTO
|
|
gptkbp:launchSite
|
gptkb:Guiana_Space_Centre
|
|
gptkbp:launchVehicle
|
Ariane_family
|
|
gptkbp:manufacturer
|
gptkb:European_Space_Agency
|
|
gptkbp:notableContestants
|
gptkb:European_Space_Research_and_Technology_Centre
|
|
gptkbp:notableEvent
|
first commercial launch of a satellite
|
|
gptkbp:notableFeature
|
gptkb:Hubble_Space_Telescope
|
|
gptkbp:numberOfEpisodes
|
multiple
|
|
gptkbp:operationalStatus
|
1979
active
up to 100 bar
|
|
gptkbp:partOf
|
European_space_launch_strategy
|
|
gptkbp:passenger_traffic
|
adaptable to various payloads
|
|
gptkbp:performance
|
measured in thrust-to-weight ratio
|
|
gptkbp:productionCompany
|
1970s
|
|
gptkbp:propulsion
|
up to 1500 kN
|
|
gptkbp:reliability
|
high
|
|
gptkbp:safetyFeatures
|
excellent
|
|
gptkbp:setting
|
staged combustion cycle
|
|
gptkbp:successor
|
Vega_rocket_engines
|
|
gptkbp:team
|
European_aerospace_engineers
|
|
gptkbp:technology
|
liquid oxygen and kerosene
|
|
gptkbp:usedIn
|
gptkb:Ariane_launch_vehicles
|