|
gptkbp:instanceOf
|
rocket engine
|
|
gptkbp:controls
|
digital control system
|
|
gptkbp:coolingSystem
|
regenerative cooling
|
|
gptkbp:designedBy
|
gptkb:Arianespace
|
|
gptkbp:developer
|
1990s
|
|
gptkbp:engineConfiguration
|
single engine configuration
|
|
gptkbp:engineType
|
liquid bipropellant
|
|
gptkbp:exhaustSystem
|
60:1
|
|
gptkbp:firstFlight
|
gptkb:Ariane_5_Flight_1
1996
2019
over 100
|
|
gptkbp:fuelType
|
staged combustion
liquid oxygen and liquid hydrogen
pyrotechnic ignition
|
|
gptkbp:hasContent
|
approximately 450 seconds
|
|
gptkbp:hasDepartment
|
approximately 600 seconds
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Vulcain engine
|
|
gptkbp:launchSite
|
Centre Spatial Guyanais
|
|
gptkbp:length
|
4.5 m
|
|
gptkbp:notableFeature
|
gptkb:BepiColombo
gptkb:Rosetta
gptkb:Mars_Express
VA253
VA245
VA246
VA248
VA249
VA252
VA256
VA258
VA259
VA261
VA263
VA264
VA265
VA266
VA268
VA269
VA270
VA241
VA243
VA244
VA240
VA242
VA247
VA250
VA251
VA254
VA255
VA257
VA260
VA262
VA267
|
|
gptkbp:numberOfMembers
|
two
|
|
gptkbp:operationalStatus
|
retired
approximately 70 bar
|
|
gptkbp:propulsion
|
1200 kN
gimbal system
|
|
gptkbp:relatedPatent
|
gptkb:Ariane_5_ELA-2
gptkb:Ariane_5_ECA
gptkb:Ariane_5_ELA-1
gptkb:Ariane_5_ELA-4
gptkb:Ariane_5_ES
gptkb:Ariane_5_ELA-3
gptkb:Ariane_5_ESTR
|
|
gptkbp:replacedBy
|
gptkb:Vulcain_2.1
|
|
gptkbp:rotorDiameter
|
2.4 m
|
|
gptkbp:successor
|
gptkb:Vulcain_2
|
|
gptkbp:usedIn
|
gptkb:Ariane_5
|
|
gptkbp:weight
|
approximately 3,000 kg
|