Ariane 5 Generic
| Main Data | Ariane 5G |
|---|---|
| Height* | 46 to 52 m |
| Diameter | up to 5.4 m |
| Liftoff mass** | 746 tonnes |
| Payload mass*** |
6 tonnes GTO 9.5 tonnes SSO |
Ariane 5 made its first successful launch on 30 October 1997. Its first operational flight took place in December 1999 when it launched ESA’s X-ray Multi-Mirror (XMM) satellite. Since it became operational Ariane 5 has been used to launch satellites for communications, Earth observation and scientific research.
In order for Ariane 5 to use Europe’s Spaceport in Kourou ESA built a new launch site as well as facilities to integrate the solid boosters and produce the solid propellant they use.
Ariane 5 is used for launches into geostationary orbit, medium and low-Earth orbits and sun-synchronous orbits.
* Double launch
Last update: 12 May 2004
Related links
- Ariane 5 Generic
http://www.esa.int/Our_Activities/Launchers/Ariane_5_generic_animation - Ariane 5 net
http://www.esa.int/Our_Activities/Launchers/Ariane_5_NET_animation - Build a launcher
http://www.esa.int/Our_Activities/Launchers/building_a_launcher_animation - Ariane 5 elements
javascript:win1() - Boosters (EAP)
http://www.esa.int/Our_Activities/Launchers/Launch_vehicles/Boosters_EAP - Cryogenic main stage (EPC)
http://www.esa.int/Our_Activities/Launchers/Launch_vehicles/Cryogenic_main_stage_EPC - Vulcain engine
http://www.esa.int/Our_Activities/Launchers/Launch_vehicles/Vulcain_engine - Storable Propellant Stage (EPS)
http://www.esa.int/Our_Activities/Launchers/Launch_vehicles/Storable_Propellant_Stage_EPS - Vehicle equipment bay
http://www.esa.int/Our_Activities/Launchers/Launch_vehicles/Vehicle_equipment_bay - Speltra, Sylda 5
http://www.esa.int/Our_Activities/Launchers/Launch_vehicles/Speltra_Sylda_5 - Fairing
http://www.esa.int/Our_Activities/Launchers/Launch_vehicles/Fairing - Space, cities and education
http://www.esa.int/Our_Activities/Launchers/Launch_vehicles/Space_cities_and_education

