ESAATVInternational Space StationHuman Spaceflight and Exploration
   
Flight plan
ATV mission conceptATV flight phasesATV cargo capacity
Spacecraft
ATV Configuration
ATV Integrated Cargo CarrierATV Service ModuleATV evolution
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ATV-1: Jules VerneATV-2: Johannes KeplerATV-3: Edoardo Amaldi
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ATV newspaper (pdf)ATV-1 Jules Verne Information Kit (pdfs)ATV-1 Jules Verne factsheet 2008 (pdf)
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ATV Configuration
 
Inside the ATV
 

The exterior of this new generation spacecraft is a cylinder, 10.3 metres long and up to 4.5 metres in diameter. The details of the ATV's external structure are covered with a foil layer and meteorite protection panels.

Characteristic x-shaped solar arrays extend from the spacecraft. Deployed 100 minutes after lift-off, the solar arrays reach a span of 22.3 m. The four arrays are totally idependent and can rotate to get the best orientation to the Sun. They are able to produce an average of 4 800 watts - providing power to rechargeable batteries which are vital for powering ATV systems when the spacecraft is in the shadow of the Earth.  
 

 
The ATV consists of two main modules:
 
 
Last update: 4 March 2010
 


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