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gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:configuration
|
gptkb:EFS_(Enhanced_Payload_Fairing_System)
|
|
gptkbp:debut
|
1996-2003
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|
gptkbp:design_purpose
|
To enable interplanetary missions
To enhance European space capabilities
To increase payload capacity
To replace Ariane 4
To support larger satellites
|
|
gptkbp:development_cost
|
$7 billion
|
|
gptkbp:diameter
|
5.4 meters
|
|
gptkbp:engine_type
|
gptkb:Vulcain
|
|
gptkbp:first_flight
|
1996-06-04
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|
gptkbp:height
|
50 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Ariane 5 EFS
|
|
gptkbp:launch_date
|
2-3 per year
|
|
gptkbp:launch_mass
|
780,000 kg
|
|
gptkbp:launch_platform
|
gptkb:Guiana_Space_Centre
|
|
gptkbp:launch_price
|
approximately $150 million
|
|
gptkbp:launch_site
|
gptkb:Centre_Spatial_Guyanais
|
|
gptkbp:launch_vehicle
|
gptkb:Ariane_5
Heavy-lift launch vehicle
Expendable launch vehicle
|
|
gptkbp:launch_window
|
varies by mission
|
|
gptkbp:manufacturer
|
gptkb:Arianespace
|
|
gptkbp:mission
|
Geostationary and interplanetary missions
|
|
gptkbp:notable_launches
|
gptkb:Herschel
gptkb:Planck
gptkb:Rosetta
gptkb:Mars_Express
|
|
gptkbp:number_of_stages
|
gptkb:Cryogenic_Upper_Stage
gptkb:Solid_Rocket_Boosters
2
|
|
gptkbp:operational_period
|
gptkb:7
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:operational_use
|
gptkb:International_collaborations
Commercial satellite launches
Scientific missions
Government payloads
|
|
gptkbp:payload_capacity
|
4.6 meters in diameter
10,500 kg to geostationary transfer orbit
|
|
gptkbp:reliability
|
high
|
|
gptkbp:significant_event
|
First commercial launch of Ariane 5
Launch of the Herschel Space Observatory
Launch of the Planck satellite
Launch of the first European Mars mission
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|
gptkbp:strategic_goals
|
gptkb:1
|
|
gptkbp:success
|
gptkb:25
|
|
gptkbp:success_rate
|
95%
|
|
gptkbp:successor
|
gptkb:Ariane_6
|
|
gptkbp:bfsParent
|
gptkb:Ariane_rockets
|
|
gptkbp:bfsLayer
|
5
|