Please make a donation to support Gunter's Space Page.
Thank you very much for visiting Gunter's Space Page. I hope that this site is useful and informative for you.
If you appreciate the information provided on this site, please consider supporting my work by making a simple and secure donation via PayPal. Please help to run the website and keep everything free of charge. Thank you very much.

ATV 1, 2, 3, 4, 5

ATV-2 [ESA]

The ATV (Autonomous Transfer Vehicle) is an unmanned, non-reusable cargo spacecraft for delivering supplies an fuel to the International Space Station.

Every 12 months the 20-tonne ATV will haul 7.5 tonnes of cargo from its Kourou launch site in French Guiana to the Station 400 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 6.5 tonnes of Station waste.

The exterior is an eggshell-coloured cylinder, 10.3 meters long and 4.5 meters in diameter. The details of the ATV's structure are covered with an insulating foil layer on top of anti-meteorite panels. The X-shaped extended solar arrays provide power. Inside, the ATV consists of two modules, the propulsion spacecraft and the integrated cargo carrier which docks with the ISS.

The 45 m³-pressurized section has room for up to eight standard racks which are loaded with modular storage cargo elements. The integrated cargo carrier also holds several tanks, containing up to 840 kg of drinking water, 860 kg of refuelling propellant for the Station's own propulsion system and 100 kg of air (oxygen and nitrogen). The ‘nose' of the cargo section contains the Russian-made docking equipment and various kinds of rendezvous sensors.

The ATV's spacecraft module navigates with four main engines (490 Newton) plus 28 smaller thrusters (220 N) for attitude control. After docking, the ATV can perform ISS attitude control, debris avoidance manoeuvres and boost the Station's orbit to overcome the effects of atmospheric drag. In order to perform this last manoeuvre the ATV uses up to 4.7 tonnes of propellant.

A typical ATV mission will begin when the craft is launched into a 300 km orbit atop an Ariane-5ES from the French Guiana equatorial launch site. Under the responsibility of the European control centre in Toulouse (France), the ATV separates from Ariane and navigation systems are activated. Thrusters are fired to boost the ATV into the transfer orbit to the ISS.

After three days of orbit adjustments, the ATV will come in sight of the ISS and will start relative navigation from about 30 km behind and 5 km below the Station. The cargo ship's computers begin final approach manoeuvres over the next two orbits, closing with ISS at walking pace.

The actual docking will be fully automatic. If there are any last-minute problems, either the ATV's computers or the Station's crew can trigger a pre-programmed sequence of anti-collision manoeuvres, which is fully independent of the main navigation system. This back-up system adds a full level of safety, which could be compared to an airbag in a car.

With the ATV securely docked, the Station's crew can enter the cargo section and remove the payload. Meanwhile, the ATV's liquid tanks will be connected to the Station's own plumbing and discharge their contents. The Station crew will manually release air components directly into the ISS's atmosphere. For up to six months, the ATV, mostly in dormant mode, will remain attached to the ISS with the hatch remaining open. The crew will steadily fill the cargo section with the Station's waste. At intervals of 10 to 45 days, the ATV's thrusters will be used to boost the Station's altitude.

Once its re-supply mission is accomplished, the ATV, filled with waste, will be closed by the crew and automatically separated. Its thrusters will use their remaining fuel to de-orbit the spacecraft to perform a controlled destructive re-entry high above the Pacific Ocean.

Nation: Europe
Type / Application: Supply
Operator: ESA
Contractors: EADS-LV, EADS Astrium → Airbus Defence and Space, Alenia Spazio → Thales Alenia
Equipment:
Configuration: Pressurised section + propulsion section
Propulsion: 4 × R-4D-11-300
Power: 4 deployable solar arrays, batteries
Lifetime: 180 days
Mass: 20750 kg (7300 kg cargo)
Orbit: 400 km × 400 km, 51.6° (typical)
Satellite COSPAR Date LS Launch Vehicle Remarks
ATV 1 (Jules Verne) 2008-008A 09.03.2008 Ko ELA-3 Ariane-5ES
ATV 2 (Johannes Kepler) 2011-007A 16.02.2011 Ko ELA-3 Ariane-5ES
ATV 3 (Edoardo Amaldi) 2012-010A 23.03.2012 Ko ELA-3 Ariane-5ES
ATV 4 (Albert Einstein) 2013-027A 05.06.2013 Ko ELA-3 Ariane-5ES
ATV 5 (Georges Lemaître) 2014-044A 29.07.2014 Ko ELA-3 Ariane-5ES

References: