|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:configuration
|
Evolved
|
|
gptkbp:debut
|
5 successful launches
|
|
gptkbp:decommissioned
|
gptkb:2003
|
|
gptkbp:design_purpose
|
to replace Ariane 4
|
|
gptkbp:development
|
gptkb:Ariane_5
|
|
gptkbp:engine
|
gptkb:Vulcain_2
|
|
gptkbp:engine_type
|
staged combustion cycle
|
|
gptkbp:failure_launches
|
gptkb:0
|
|
gptkbp:first_flight
|
2002-06-21
|
|
gptkbp:fuel_type
|
liquid oxygen and liquid hydrogen
|
|
gptkbp:guidance_system
|
inertial guidance system
|
|
gptkbp:height
|
50.5 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Ariane 5 ME
|
|
gptkbp:launch_date
|
1-2 per year
|
|
gptkbp:launch_mass
|
780,000 kg
|
|
gptkbp:launch_platform
|
gptkb:European_Space_Agency
Arianespace control center
|
|
gptkbp:launch_price
|
approximately $150 million
|
|
gptkbp:launch_site
|
gptkb:Centre_Spatial_Guyanais
|
|
gptkbp:launch_vehicle
|
ME
high performance
European design
heavy-lift launch vehicle
commercial satellite launch
Ariane family
heavy-lift specifications
part of Ariane program
successor to Ariane 4
|
|
gptkbp:launch_vehicle_end_of_service
|
gptkb:2003
|
|
gptkbp:launched
|
gptkb:5
|
|
gptkbp:manufacturer
|
gptkb:Arianespace
|
|
gptkbp:mission
|
GTO missions
|
|
gptkbp:notable_achievements
|
first successful launch of Herschel and Planck
|
|
gptkbp:notable_launches
|
Herschel and Planck missions
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:operational_period
|
2002-2003
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:orbital_insertion_accuracy
|
< 100 km
|
|
gptkbp:payload_capacity
|
5.4 meters
geostationary transfer orbit
multiple payloads
10,500 kg to GTO
integrated payload fairing
|
|
gptkbp:primary_function
|
gptkb:Space_Launch_System
|
|
gptkbp:propulsion
|
1,000 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:success
|
gptkb:5
|
|
gptkbp:success_rate
|
100%
|
|
gptkbp:successor
|
gptkb:Ariane_6
|
|
gptkbp:technology
|
advanced avionics
|
|
gptkbp:bfsParent
|
gptkb:Ariane_5
|
|
gptkbp:bfsLayer
|
4
|