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Saturn A-1, studied in 1959, was projected to be the first version of Saturn I and was to be used if necessary before the S-IV liquid hydrogen second stage became available. The first stage, proposed for the Juno V rocket, but finally used for the first Saturn rocket, would propel the Saturn A-1 into space, with the first stage of a Titan I missile continuing the flight and finally, a Centaur C high-energy double-engine third stage could perform a small burn to send a payload into its final orbit, or it can perform a big burn to take a payload out of Earth orbit to other planets. This rocket never flew, but all stages of the Saturn A-1 were used on different launch vehicles. Today, they are all retired.

AttributesValues
rdf:type
rdfs:label
  • Saturn A-1 (en)
rdfs:comment
  • Saturn A-1, studied in 1959, was projected to be the first version of Saturn I and was to be used if necessary before the S-IV liquid hydrogen second stage became available. The first stage, proposed for the Juno V rocket, but finally used for the first Saturn rocket, would propel the Saturn A-1 into space, with the first stage of a Titan I missile continuing the flight and finally, a Centaur C high-energy double-engine third stage could perform a small burn to send a payload into its final orbit, or it can perform a big burn to take a payload out of Earth orbit to other planets. This rocket never flew, but all stages of the Saturn A-1 were used on different launch vehicles. Today, they are all retired. (en)
foaf:name
  • Saturn A-1 (en)
name
  • Saturn A-1 (en)
dct:subject
Wikipage page ID
Wikipage revision ID
Link from a Wikipage to another Wikipage
sameAs
sites
  • N/A (en)
stage1engines
stage1fuel
stage1name
stage1thrust
  • 7,582 kN (en)
stage1time
stage2engines
stage2fuel
  • RP-1/LOX (en)
stage2name
stage2thrust
  • 1,467 kN (en)
stage2time
stage3engines
stage3fuel
stage3name
  • Centaur C (en)
stage3thrust
  • 133 kN (en)
stage3time
dbp:wikiPageUsesTemplate
diameter
  • 6.52 m (en)
height
  • 49.62 m (en)
manufacturer
  • Von Braun (en)
mass
status
  • Never flown (en)
stages
has abstract
  • Saturn A-1, studied in 1959, was projected to be the first version of Saturn I and was to be used if necessary before the S-IV liquid hydrogen second stage became available. The first stage, proposed for the Juno V rocket, but finally used for the first Saturn rocket, would propel the Saturn A-1 into space, with the first stage of a Titan I missile continuing the flight and finally, a Centaur C high-energy double-engine third stage could perform a small burn to send a payload into its final orbit, or it can perform a big burn to take a payload out of Earth orbit to other planets. This rocket never flew, but all stages of the Saturn A-1 were used on different launch vehicles. Today, they are all retired. (en)
alt-diameter
alt-height
country-origin
  • United States (en)
function
  • Uncrewed launch vehicle (en)
rocket function
prov:wasDerivedFrom
diameter (μ)
height (mm)
mass (kg)
mass (kg)
page length (characters) of wiki page
diameter (μ)
height (μ)
mass (g)
status
  • Never flown
number of rocket stages
foaf:isPrimaryTopicOf
is Link from a Wikipage to another Wikipage of
is foaf:primaryTopic of
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