![]() |
ATV cargo capacity
The weights are calculated for each mission depending on the cargo need, but in general the total ATV net cargo capacity can be allocated as follows (of course not all the maximum quantities presented here can be carried at once on the same flight): Wet cargo
Propulsive support propellant (up to 4.0 tonnes)
Once attached to the Station, up to 860 kg of refuelling propellant can be transferred from the ATV to the ISS. This consists of two different fluids: the fuel unsymmetrical dimethylhydrazine (UDMH) and the oxidiser, nitrogen tetroxide (N2O4), which provides a source of oxygen so the fuel can ignite and burn in orbit. This is used by the ISS for orbit and attitude control with its own engines.
Water (up to 855 kg)
Gases (up to 102 kg) Dry cargo Up to 3.2 tonnes of dry cargo can be transported to the ISS inside the Integrated Cargo Carrier of the ATV. This may include food for the crew, spare parts, clothing, and a number of additional items.
ATV Johannes Kepler had a maximum launch mass of 20 010 kg. The total net cargo (fluid and dry) load to be transported to the ISS was 7085 kg, including 1170 kg dry cargo, 100 kg oxygen, 851 kg of refuel propellant and 4535 kg of fuel for propulsive support of the ISS. In addition, up to 430 kg of late cargo, packed in 28 bags, were lowered into ATV’s cargo compartment just before launch via a manually operated winch. Dry cargo includes one small cargo transfer bag (about 13 kg each), a ‘crew care package’, for each ISS astronaut. Bags are filled with personal items such as family photos, CDs with music, chocolate or other candy.
The ATV-2 spacecraft itself has a 'dry mass' of about 9800 kg. Last update: 16 June 2011
| ||||||||||||||||||||||||