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Launch window: Feb 15, 2010. Excat launch time comes later.
Launch site: ELA-3, Kourou, French Guiana
The Arianespace Ariane 5 rocket will launch the European Space Agency's second Automated Transfer Vehicle, named Johannes Kepler. The ATV is a cargo-carrying spacecraft to deliver supplies and equipment to the orbiting International Space Station.
ATV Wikipedia Article: http://en.wikipedia.org/wiki/Automated_Transfer_Vehicle
ATV-002 (Johannes Kepler) Wikipedia Article: http://en.wikipedia.org/wiki/Johannes_Kepler_ATV
EADS Astrium ATV Page: http://cs.astrium.eads.net/sp/Spacecraf ... se/ATV.htm
Ariane 5/ATV Launch Animation:
[youtube]http://www.youtube.com/watch?v=KYI_0rzgj0E[/youtube]
Ariane 5ES Launch Vehicle (also known as Ariane 5 ES-ATV)
Arianespace's Ariane 5 Page: http://www.arianespace.com/launch-servi ... -intro.asp
Ariane 5 Wikipedia Article: http://en.wikipedia.org/wiki/Ariane_5
Ariane 5 Launch vehicle's technology: http://www.le-webmag.com/article.php3?i ... 20&lang=en
ESA's Ariane 5 Detailed Information Page: http://esamultimedia.esa.int/multimedia ... riane.html
The Main Cryogenic Stage
Ariane 5 ECA has one Vulcain II Main Engine burning LH[sub]2[/sub]/LOX
Vulcain Wikipedia Article: http://en.wikipedia.org/wiki/Vulcain
Vulcain-2 Volvo Aero Product Guide: http://www.volvoaero.com/SiteCollection ... 2_2005.pdf
Volvo Aero Vulcain 2 Product Page: http://www.volvoaero.com/VOLVOAERO/GLOB ... ain_2.aspx
Snecma Vulcain 2 Marketing Brochure: http://www.snecma.com/IMG/pdf/Brochure_ ... pdf#page=7
Snecma Vulcain 2 Technical Sheet: http://www.snecma.com/IMG/pdf/VULCAIN_2_ang-2.pdf
Snecma Vulcain 2 Product Page: http://www.snecma.com/spip.php?article121&lang=en
Solid Rocket Boosters
Arianespace's Booster Manufacturing Page: http://www.arianespace.com/spaceport-ar ... ooster.asp
Booster Test Stand Page: http://www.cnes.fr/web/CNES-en/2887-ari ... -stand.php
Booster Manufacturer: http://www.aviogroup.com/en/avio_heritage/spazio (AvioGroup, FiatAvio, Regulus)
Second Stage
One Aestus engine burning N[sub]2[/sub]O[sub]4[/sub]/MMH
EADS Astrium Aestus Page: http://cs.astrium.eads.net/sp/LauncherP ... ngine.html
EADS Astrium Aestus Brochure: http://cs.astrium.eads.net/sp/LauncherP ... aestus.pdf
Guiana Launch Centre
Guiana Wikipedia Article: http://en.wikipedia.org/wiki/Guiana_Space_Centre
Cnes CSG Official Page: http://www.cnes-csg.fr/web/CNES-CSG-en/ ... ersion.php
ESA's Europe's Spaceport Page: http://www.esa.int/SPECIALS/Launchers_E ... index.html
Google Maps: http://maps.google.com/maps?t=h&q=5.237 ... 55575&z=15
Launch site: ELA-3, Kourou, French Guiana
The Arianespace Ariane 5 rocket will launch the European Space Agency's second Automated Transfer Vehicle, named Johannes Kepler. The ATV is a cargo-carrying spacecraft to deliver supplies and equipment to the orbiting International Space Station.
ATV Wikipedia Article: http://en.wikipedia.org/wiki/Automated_Transfer_Vehicle
ATV-002 (Johannes Kepler) Wikipedia Article: http://en.wikipedia.org/wiki/Johannes_Kepler_ATV
EADS Astrium ATV Page: http://cs.astrium.eads.net/sp/Spacecraf ... se/ATV.htm
Ariane 5/ATV Launch Animation:
[youtube]http://www.youtube.com/watch?v=KYI_0rzgj0E[/youtube]
Ariane 5ES Launch Vehicle (also known as Ariane 5 ES-ATV)
Arianespace's Ariane 5 Page: http://www.arianespace.com/launch-servi ... -intro.asp
Ariane 5 Wikipedia Article: http://en.wikipedia.org/wiki/Ariane_5
Ariane 5 Launch vehicle's technology: http://www.le-webmag.com/article.php3?i ... 20&lang=en
ESA's Ariane 5 Detailed Information Page: http://esamultimedia.esa.int/multimedia ... riane.html
The Main Cryogenic Stage
Arianespace Web Pages":1j3nw57z said:As the central element of Ariane 5, the core cryogenic stage serves as one of the launcher's key propulsion systems.
It carries a propellant load of 132.27 metric tons of liquid oxygen and 25.84 metric tons of liquid hydrogen to feed the stage's Vulcain main engine.
The Vulcain burns for just under 600 seconds, providing up to 116 metric tons of thrust in vacuum.
The stage has an overall length of 30.5 meters from the Vulcain main engine's nozzle to the forward (upper) skirt.
Its dry mass is 12.2 metric tons, and the liftoff mass with its load of cryogenic propellant is 170.3 metric tons.
After completing its propulsive mission, the empty stage is commanded to reenter the atmosphere for an ocean splashdown.
Ariane 5 ECA has one Vulcain II Main Engine burning LH[sub]2[/sub]/LOX
Vulcain Wikipedia Article: http://en.wikipedia.org/wiki/Vulcain
Vulcain-2 Volvo Aero Product Guide: http://www.volvoaero.com/SiteCollection ... 2_2005.pdf
Volvo Aero Vulcain 2 Product Page: http://www.volvoaero.com/VOLVOAERO/GLOB ... ain_2.aspx
Snecma Vulcain 2 Marketing Brochure: http://www.snecma.com/IMG/pdf/Brochure_ ... pdf#page=7
Snecma Vulcain 2 Technical Sheet: http://www.snecma.com/IMG/pdf/VULCAIN_2_ang-2.pdf
Snecma Vulcain 2 Product Page: http://www.snecma.com/spip.php?article121&lang=en
Solid Rocket Boosters
Arianespace's Booster Manufacturing Page: http://www.arianespace.com/spaceport-ar ... ooster.asp
Booster Test Stand Page: http://www.cnes.fr/web/CNES-en/2887-ari ... -stand.php
Booster Manufacturer: http://www.aviogroup.com/en/avio_heritage/spazio (AvioGroup, FiatAvio, Regulus)
Arianespace Web Pages":1j3nw57z said:Ariane 5 utilizes two solid boosters, each standing more than 30 meters tall with 237.8 metric tons of propellant. The boosters are ignited on the launch pad once the main cryogenic stage's Vulcain engine has stabilized its thrust output.
They deliver more than 90 percent of the launcher's total thrust at the start of flight and burn for 130 sec. before they are separated over a designated zone of the Atlantic Ocean.
The booster stage’s solid rocket motor is made up of three segments: the 11.1-meter-long aft (lower) segment, which is loaded with 106.7 metric tons of propellant; the center segment, with a length of 10.17 meters and 107.4 metric tons of propellant; and the 3.5-meter-long forward (upper) segment, loaded with 23.4 metric tons of propellant.
A propellant mix of 68 percent ammonium perchlorate (oxidizer), 18 percent aluminum (fuel), and 14 percent polybutadiene (binder) is used in the solid rocket motors.
The combustion process is initiated by a pyrotechnic device, and the solid propellant burns at a radial velocity (from the center outward) of approximately 7.4 mm/sec.
Flight control is provided by the boosters' movable nozzle, which is driven by hydraulically-controlled servoactuators.
Second Stage
One Aestus engine burning N[sub]2[/sub]O[sub]4[/sub]/MMH
EADS Astrium Aestus Page: http://cs.astrium.eads.net/sp/LauncherP ... ngine.html
EADS Astrium Aestus Brochure: http://cs.astrium.eads.net/sp/LauncherP ... aestus.pdf
Guiana Launch Centre
Guiana Wikipedia Article: http://en.wikipedia.org/wiki/Guiana_Space_Centre
Cnes CSG Official Page: http://www.cnes-csg.fr/web/CNES-CSG-en/ ... ersion.php
ESA's Europe's Spaceport Page: http://www.esa.int/SPECIALS/Launchers_E ... index.html
Google Maps: http://maps.google.com/maps?t=h&q=5.237 ... 55575&z=15