|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:collaboration
|
ESA and CNES
|
|
gptkbp:configuration
|
Evolved
|
|
gptkbp:debut
|
2002-2013
30 successful launches
|
|
gptkbp:design_purpose
|
heavy-lift launch vehicle
|
|
gptkbp:designed_for
|
heavy payloads
|
|
gptkbp:development
|
gptkb:European_Space_Agency
|
|
gptkbp:development_cost
|
7 billion euros
|
|
gptkbp:diameter
|
5.4 meters
|
|
gptkbp:engine
|
gptkb:Vulcain_2
|
|
gptkbp:engine_configuration
|
Single Vulcain 2 engine
|
|
gptkbp:engine_type
|
gptkb:Vulcain_2
|
|
gptkbp:first_flight
|
July 4, 2013
2013-10-25
December 11, 2002
2002-12-12
|
|
gptkbp:fuel_type
|
Liquid oxygen and liquid hydrogen
|
|
gptkbp:guidance_system
|
Inertial navigation system
|
|
gptkbp:height
|
50 meters
50.5 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Ariane 5 ECA
|
|
gptkbp:launch_date
|
approximately 30 minutes
approximately 2 per year
|
|
gptkbp:launch_event
|
100% for commercial missions
|
|
gptkbp:launch_mass
|
780,000 kg
|
|
gptkbp:launch_platform
|
gptkb:Arianespace
|
|
gptkbp:launch_price
|
150 million euros
|
|
gptkbp:launch_site
|
gptkb:Centre_Spatial_Guyanais
|
|
gptkbp:launch_vehicle
|
gptkb:Ariane_5
2
Expendable launch vehicle
Expendable launch system
Evolved version of Ariane 5
|
|
gptkbp:launched
|
gptkb:the_Planck_satellite
gptkb:30
gptkb:Kourou,_French_Guiana
multiple satellites
the Herschel Space Observatory
|
|
gptkbp:manufacturer
|
gptkb:Arianespace
|
|
gptkbp:mass
|
780,000 kg
|
|
gptkbp:mission
|
Launch of the Alphasat satellite.
|
|
gptkbp:notable_achievements
|
First launch of a European satellite to GTO
|
|
gptkbp:notable_launches
|
gptkb:Herschel_Space_Observatory
gptkb:Planck_satellite
|
|
gptkbp:notable_mission
|
launching the Amazonas satellites
launching the Astra satellites
launching the Bepi Colombo mission
launching the Eutelsat satellites
launching the Galileo satellites
launching the Hispasat satellites
launching the Intelsat satellites
launching the MEASAT satellites
launching the SES satellites
launching the Turksat satellites
|
|
gptkbp:number_of_stages
|
gptkb:Cryogenic_Upper_Stage
gptkb:Solid_Rocket_Boosters
2
|
|
gptkbp:operated_by
|
gptkb:European_Space_Agency
|
|
gptkbp:operational_period
|
2002-2013
11 years
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:operational_use
|
commercial satellite launches
|
|
gptkbp:orbital_inclination
|
gptkb:GTO
|
|
gptkbp:part_of
|
Ariane family
|
|
gptkbp:payload_capacity
|
Geostationary orbit
10,500 kg
4.6 meters
6,900 kg
|
|
gptkbp:payload_configuration
|
Single or dual payloads
|
|
gptkbp:primary_use
|
gptkb:Space_Launch_System
|
|
gptkbp:propulsion
|
1,000 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:retired
|
gptkb:2013
|
|
gptkbp:strategic_goals
|
gptkb:0
|
|
gptkbp:success
|
gptkb:25
|
|
gptkbp:success_rate
|
95%
|
|
gptkbp:successfully_completed_missions
|
gptkb:30
|
|
gptkbp:successor
|
gptkb:Ariane_6
|
|
gptkbp:used_for
|
satellite launches
|
|
gptkbp:weight
|
780,000 kg
|
|
gptkbp:bfsParent
|
gptkb:James_Webb_Space_Telescope
gptkb:Ariane_5
|
|
gptkbp:bfsLayer
|
4
|