About: Atlas II

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Atlas II was a member of the Atlas family of launch vehicles, which evolved from the successful Atlas missile program of the 1950s. Atlas II was the last Atlas to use a three engine, "stage-and-a-half" design: two of its three engines were jettisoned during ascent, but its fuel tanks and other structural elements were retained. It was designed to launch payloads into low earth orbit, geosynchronous transfer orbit or geosynchronous orbit.

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rdfs:comment	Atlas II was a member of the Atlas family of launch vehicles, which evolved from the successful Atlas missile program of the 1950s. Atlas II was the last Atlas to use a three engine, "stage-and-a-half" design: two of its three engines were jettisoned during ascent, but its fuel tanks and other structural elements were retained. It was designed to launch payloads into low earth orbit, geosynchronous transfer orbit or geosynchronous orbit.
foaf:name	Atlas II
foaf:depiction
country origin	United States
diameter (μ)	3(xsd:double)
final flight	1998-03-16(xsd:dateTime) 2002-12-05(xsd:dateTime) 2004-08-31(xsd:dateTime)
height (μ)	47(xsd:double)
launch site	80px SLC-3 Launch Complex 36
lower earth orbit payload (g)	6580000(xsd:double)
maiden flight	1991-12-07(xsd:dateTime) 1992-06-10(xsd:dateTime) 1993-12-16(xsd:dateTime)
manufacturer	Lockheed Martin
mass (g)	204300000(xsd:double)
rocket function	dbpedia:Launch_vehicle
number of rocket stages	4(xsd:integer)
status	Retired
successful launches	10(xsd:integer) 63(xsd:integer)
thumbnail	http://commons.wikimedia.org/wiki/Special:FilePath/DF-SC-99-00074_cropped_and_rotated.jpeg?width=300
total launches	10(xsd:integer) 63(xsd:integer)
is maiden flight rocket of	dbpedia:1993_in_spaceflight dbpedia:1991_in_spaceflight dbpedia:1992_in_spaceflight
is retired rocket of	dbpedia:2004_in_spaceflight dbpedia:2002_in_spaceflight dbpedia:1998_in_spaceflight

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