 |  |  |  |  |
| |  | |  | |
 |
Flight plan ATV mission conceptATV flight phasesATV cargo capacitySpacecraft ATV configurationATV Integrated Cargo CarrierATV Service ModuleATV evolutionATV Missions ATV-1: Jules VerneATV-2: Johannes KeplerATV-3: Edoardo AmaldiATV-4: Albert EinsteinOperations Flight operationsATV Control CentreCrew roleIndustry ESA's roleEuropean industryDownloads ATV Edoardo Amaldi factsheet (pdf)ATV Edoardo Amaldi info kit English (pdf)ATV Edoardo Amaldi info kit German (pdf)ATV Edoardo Amaldi info kit French (pdf)ATV Edoardo Amaldi info kit Italian (pdf)ATV: Servicing the International Space Station (pdf)Multimedia gallery ATV image galleryATV video galleryServices
|  |  |  |  | | | |  | The Automated Transfer Vehicle (ATV) | | Automated Transfer Vehicle (ATV)
European servicing and logistics vehicle
The International Space Station (ISS) depends on regular deliveries of experimental equipment and spare parts as well as food, air and water for its permanent crew. From early 2008 onward, Europe's Automated Transfer Vehicle (ATV) will be one of the indispensable ISS supply spaceships. Every 12 months or so, the ATV will haul 7.7 tonnes of cargo from its Kourou launch site in French Guiana to the Station 340 km above the Earth. An on board high precision navigation system will guide the ATV on a rendezvous trajectory towards ISS, where it will automatically dock with the Station's Russian service module. The ATV will remain there as a pressurized and integral part of the Station for up to six months until its final mission: a fiery one-way trip into the Earth's atmosphere to dispose of up to 6.4 tonnes of Station waste.
| Dimensions | | | Length: | 9 794 mm | | Largest diameter: | 4 480 mm | | Solar arrays span: | 22 281 mm | | Mass budget | | | Vehicle dry mass: | 10 470 kg | | Vehicle consumables: | 2 613 kg | | Total vehicle mass: | 13 083 kg | | Total cargo upload capacity: | 7 667 kg | | Mass at launch: | 19 357 kg | | Waste download capacity: | 6 400 kg | | | |
| | Launch configuration | | | Cargo mass capabilities | Dry supplies: 5 500 kg | | | Drinking water: 840 kg | | | Air (oxygen and nitrogen): 100 kg | | | ISS refuelling propellant: 860 kg | | | ISS re-boost and attitude control propellant: 4 700 kg | | | Total cargo upload capacity: 7 667 kg | | Launch vehicle | Ariane 5 ES ATV (inclination 51.6°; initial orbital altitude 260 km) | | | ATV will be launched with its solar panels folded to the body of the spacecraft | | Launch site | Kourou, French Guiana | | First flight | 9 March 2008 | | | |
| Last update: 16 January 2009 | |
|  | More information Automated Transfer Vehicle (ATV)ATV Jules Verne factsheet 2008 (pdf)
|