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gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:application
|
gptkb:Space_Launch_System
|
|
gptkbp:check_in_time
|
600 seconds
|
|
gptkbp:combustor_type
|
staged combustion
|
|
gptkbp:control_system
|
digital control system
|
|
gptkbp:cooling_system
|
film cooling
|
|
gptkbp:design
|
15 years
|
|
gptkbp:development
|
gptkb:Ariane_4
gptkb:1984
|
|
gptkbp:diameter
|
2.6 m
|
|
gptkbp:engine
|
gptkb:European_Space_Agency
staged combustion cycle
influenced future rocket designs
controlled shutdown
ground test
advanced cryogenic technology
part of European space launch history
|
|
gptkbp:engine_configuration
|
detailed specifications available
single engine
|
|
gptkbp:engine_power
|
optimized for heavy payloads
|
|
gptkbp:engine_type
|
gptkb:Vulcain_2.1
cryogenic engine
|
|
gptkbp:environmental_impact
|
low emissions
|
|
gptkbp:exhaust_system
|
expander nozzle
|
|
gptkbp:first_flight
|
gptkb:1996
gptkb:2019
|
|
gptkbp:flight_style
|
253
|
|
gptkbp:fuel_type
|
liquid hydrogen
liquid oxygen and liquid hydrogen
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Arianespace Vulcain engine
|
|
gptkbp:ignition_system
|
pyrotechnic
|
|
gptkbp:is_tested_for
|
extensive testing program
|
|
gptkbp:launch_mass
|
over 700 tons
|
|
gptkbp:launch_site
|
gptkb:Centre_Spatial_Guyanais
|
|
gptkbp:length
|
4.5 m
|
|
gptkbp:manufacturer
|
gptkb:Arianespace
|
|
gptkbp:number_of_rooms
|
gptkb:1
180 bar
|
|
gptkbp:number_of_stages
|
gptkb:Ariane_5
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:operational_use
|
commercial satellite launches
|
|
gptkbp:oxidation_states
|
liquid oxygen
|
|
gptkbp:part_of
|
Ariane family
|
|
gptkbp:propulsion
|
40:1
1200 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:successor
|
gptkb:Vulcain_2
|
|
gptkbp:used_in
|
gptkb:Ariane_5
|
|
gptkbp:weight
|
3000 kg
|
|
gptkbp:bfsParent
|
gptkb:AR1_rocket_engine
|
|
gptkbp:bfsLayer
|
6
|