Statements (55)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
rocket engine
|
| gptkbp:annualRidership |
over 50
|
| gptkbp:barrelLength |
90 bar
|
| gptkbp:construction_cost |
significant investment
|
| gptkbp:coolingSystem |
regenerative cooling
efficient cooling system |
| gptkbp:design_feature |
advanced materials
|
| gptkbp:developer |
Ariane_5_program
|
| gptkbp:documentType |
expanding nozzle
|
| gptkbp:engine |
modular design
large size various space missions new technologies implemented conducted before flights focus on efficiency and reliability influential in rocket design retired after successful service |
| gptkbp:engineConfiguration |
single engine
mass production techniques used |
| gptkbp:engineType |
liquid bipropellant engine
|
| gptkbp:environmental_impact |
low emissions
|
| gptkbp:firstFlight |
1996
|
| gptkbp:fuel_capacity |
high efficiency
|
| gptkbp:fuelType |
staged combustion
liquid oxygen and liquid hydrogen pyrotechnic |
| gptkbp:hasArea |
gptkb:Guiana_Space_Centre
extensive ground testing |
| gptkbp:hasDepartment |
about 600 seconds
|
| https://www.w3.org/2000/01/rdf-schema#label |
Vulcain 2.1E
|
| gptkbp:inspiration |
high reliability
|
| gptkbp:is_designed_to |
gptkb:Ariane_5
|
| gptkbp:launchDate |
successful launches
regular launches |
| gptkbp:launchSite |
Centre Spatial Guyanais
|
| gptkbp:launchVehicle |
gptkb:Ariane_5_ECA
|
| gptkbp:manufacturer |
ArianeGroup
|
| gptkbp:number_of_stages |
single stage
|
| gptkbp:operational_status |
retired
commercial satellite launches launching satellites |
| gptkbp:performances |
high reliability rating
detailed technical specifications measured during flights optimized for payload delivery |
| gptkbp:productionYears |
1996 to 2019
|
| gptkbp:propulsion |
yes
450 seconds 1300 kN 1300 kN at sea level over 400:1 |
| gptkbp:related_engine |
gptkb:European_Space_Agency
staged combustion cycle |
| gptkbp:successor |
gptkb:Vulcain_2.0
|
| gptkbp:weight |
approximately 3,000 kg
|