|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:check_in_time
|
approximately 600 seconds
|
|
gptkbp:combustor_type
|
staged combustion
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:designed_for
|
gptkb:Ariane_5
|
|
gptkbp:developed_by
|
gptkb:Arianespace
|
|
gptkbp:development_cost
|
approximately €1 billion
|
|
gptkbp:engine
|
staged combustion cycle
|
|
gptkbp:engine_configuration
|
single nozzle
|
|
gptkbp:engine_nozzle_type
|
converging-diverging nozzle
|
|
gptkbp:engine_power
|
high
optimized for heavy payloads
|
|
gptkbp:engine_type
|
liquid bipropellant
|
|
gptkbp:first_flight
|
gptkb:Ariane_5_flight_1
gptkb:1996
gptkb:2020
|
|
gptkbp:fuel_capacity
|
3.8 m
5.4 m
|
|
gptkbp:fuel_economy
|
250 kg/s
|
|
gptkbp:fuel_type
|
liquid oxygen and liquid hydrogen
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Vulcain 2
|
|
gptkbp:ignition_system
|
pyrotechnic
|
|
gptkbp:is_tested_for
|
performed at the DLR
|
|
gptkbp:launch_site
|
gptkb:Centre_Spatial_Guyanais
|
|
gptkbp:manufacturer
|
gptkb:Snecma
|
|
gptkbp:mission
|
multiple Ariane 5 launches
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:number_of_rooms
|
180 bar
|
|
gptkbp:operational_since
|
gptkb:2002
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:operational_use
|
commercial satellite launches
|
|
gptkbp:oxidizer_consumption
|
1,000 kg/s
|
|
gptkbp:part_of
|
Ariane family
|
|
gptkbp:propulsion
|
yes
400:1
1200 k N
|
|
gptkbp:replaced_by
|
gptkb:Vulcain_2.1
|
|
gptkbp:specific_impulse
|
450 seconds in vacuum
|
|
gptkbp:successor
|
gptkb:Vulcain_1
|
|
gptkbp:used_in
|
gptkb:Ariane_5_EFS
gptkb:Ariane_5_ECA
gptkb:Ariane_5_ES
gptkb:Ariane_5_GS
gptkb:Ariane_5_ME
Ariane 5 ECA+.
|
|
gptkbp:weight
|
approximately 3,000 kg
|
|
gptkbp:bfsParent
|
gptkb:Ariane_5_ECA+
gptkb:Ariane_5_EAP
gptkb:Vulcain_engine
gptkb:Ariane_5_ECA
gptkb:Ariane_5_G
gptkb:Ariane_5_GS
gptkb:Ariane_5_ME
|
|
gptkbp:bfsLayer
|
5
|