ATV-2 Diagram.jpg

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DescriptionATV-2 Diagram.jpg	English: ATV-2 • The ATV is about the size of a traditional London double-decker bus. • Propulsion Module. It has four main engines and 20 smaller thrusters for attitude control. • Docking and refuelling system. The „nose“ contains the rendezvous sensors and Russian-made docking equipment. It also has eight thrusters to complement the propulsion system. • Integrated Cargo Carrier. Attaches directly to the space station and can store up to eight standard payload racks. • Four solar arrays. Provide electrical power to rechargeable batteries for eclipse periods. ATV can fully operate with the 4800 W generated by its solar wings, equivalent to the electricity used by a typical water heater at home. • Protection Panels. Protect against micrometeoroid and orbital debris. Cargo Payload – 4.4 tons of propellant (reboost and attitude control propellant) – 1,896 pounds of refuelling propellant for the station’s propulsion system – 220 pounds of air (oxygen and nitrogen) – 1.76 tons of dry supplies like bags, drawers and fresh food Total: 7 tons Measurements Largest diameter: 14.7 feet Length (probe retracted): 32.13 feet Total vehicle mass: 28,843 pounds Solar arrays span: 73.16 feet
Date	October 2010
Source	http://www.nasa.gov/mission_pages/station/expeditions/expedition26/index.html PDF
Author	NASA

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	Date/Time	Thumbnail	Dimensions	User	Comment
current	17:02, 2 November 2010		559 × 545 (35 KB)	wikimediacommons>Ras67	{{Information \|Description={{en\|1='''''ATV-2''''' • The ATV is about the size of a traditional London double-decker bus. • Propulsion Module. It has four main engines and 20 smaller thrusters for attitude control. • Docking and refuelling system.

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