About: Atlas II   Sponge Permalink

An Entity of Type : dbkwik:resource/8l4XF1POLNOQaOEfb93EaQ==, within Data Space : 134.155.108.49:8890 associated with source dataset(s)

Atlas II was a member of the Atlas family of launch vehicles, which evolved from the successful Atlas missile program of the 1950s. It was designed to launch payloads into low earth orbit, geosynchronous transfer orbit or geosynchronous orbit. Sixty-three launches of the Atlas II, IIA and IIAS models were carried out between 1991 and 2004; all sixty-three launches were successes, making the Atlas II the most reliable launch system in history. The Atlas line was continued by the Atlas III, used between 2000 and 2005, and the Atlas V which is still in use.

AttributesValues
rdf:type
rdfs:label
  • Atlas II
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. It was designed to launch payloads into low earth orbit, geosynchronous transfer orbit or geosynchronous orbit. Sixty-three launches of the Atlas II, IIA and IIAS models were carried out between 1991 and 2004; all sixty-three launches were successes, making the Atlas II the most reliable launch system in history. The Atlas line was continued by the Atlas III, used between 2000 and 2005, and the Atlas V which is still in use.
sameAs
dcterms:subject
dbkwik:nasa/proper...iPageUsesTemplate
dbkwik:scratch-pad...iPageUsesTemplate
dbkwik:scratchpad/...iPageUsesTemplate
alt-boostersthrust
  • 2,093.3 kN
success
  • 63(xsd:integer)
alt-stage3thrust
  • 220(xsd:integer)
sites
launches
  • 63(xsd:integer)
Payload
  • 2810.0
diameter
  • 3.04 m
stage2time
  • 392.0
boostertime
  • 56.0
Last
  • --03-16
  • --08-31
  • --12-05
stage1time
  • 283.0
boosterengines
  • 1(xsd:integer)
boostername
  • Castor 4A
Status
  • Retired
stage3engines
  • 1(xsd:integer)
stage2SI
  • 449.0
stage3time
  • 60.0
stage2thrust
  • 147 kN
payloads
Name
  • Atlas II
imsize
  • 270(xsd:integer)
alt-height
  • 156.0
Caption
  • Launch of an Atlas II rocket
First
  • --06-10
  • --12-16
  • --12-07
Function
  • Medium expendable Launch vehicle
country-origin
  • United States
stage2name
alt-diff
  • all
LEO-payload
  • 6580.0
stage3thrust
  • 980.0
alt-boostername
boosterSI
  • 266.0
boosterfuel
Mass
  • 204300.0
Stages
  • 3(xsd:double)
Height
  • 47.54 m
Manufacturer
  • Lockheed Martin
alt-boostertime
  • 172.0
alt-diameter
  • 10.0
stage1SI
  • 316.0
boosterthrust
  • 478.3 kN
alt-alt-boosterthrust
  • 470680(xsd:integer)
Diff
  • Atlas IIAS
alt-stage1thrust
  • 86844(xsd:integer)
stage1thrust
  • 386 kN
stage2fuel
stage3fuel
alt-boosters
  • 1(xsd:integer)
stage1fuel
alt-boosterSI
  • 299.0
stage3name
payload-location
alt-boosterengines
  • 2(xsd:integer)
alt-mass
  • 414000.0
boosters
  • 4(xsd:integer)
Family
stage3SI
  • 312.0
alt-boosterthrust
  • 107530(xsd:integer)
alt-boosterfuel
stage2engines
  • 2(xsd:integer)
stage1engines
  • 1(xsd:integer)
alt-stage2thrust
  • 41592(xsd:integer)
abstract
  • Atlas II was a member of the Atlas family of launch vehicles, which evolved from the successful Atlas missile program of the 1950s. It was designed to launch payloads into low earth orbit, geosynchronous transfer orbit or geosynchronous orbit. Sixty-three launches of the Atlas II, IIA and IIAS models were carried out between 1991 and 2004; all sixty-three launches were successes, making the Atlas II the most reliable launch system in history. The Atlas line was continued by the Atlas III, used between 2000 and 2005, and the Atlas V which is still in use.
is launch rocket of
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