Saturn A-1

http://dbpedia.org/resource/Saturn_A-1 an entity of type: Thing

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. rdf:langString

rdfs:label

rdf:langString Saturn A-1

foaf:name

rdf:langString Saturn A-1

dbpprop:name

rdf:langString Saturn A-1

dbpedia-owl:wikiPageID

xsd:integer 10700211

dbpedia-owl:wikiPageRevisionID

xsd:integer 948958819

dbpprop:sites

rdf:langString N/A

dbpprop:stage1engines

xsd:integer 8

dbpprop:stage1thrust

rdf:langString 7,582 kN

dbpprop:stage1time

<second> 150.0

dbpprop:stage2engines

xsd:integer 2

dbpprop:stage2fuel

rdf:langString RP-1/LOX

dbpprop:stage2thrust

rdf:langString 1,467 kN

dbpprop:stage2time

<second> 138.0

dbpprop:stage3engines

xsd:integer 2

dbpprop:stage3name

rdf:langString Centaur C

dbpprop:stage3thrust

rdf:langString 133 kN

dbpprop:stage3time

<second> 430.0

dbpprop:diameter

rdf:langString 6.52 m

dbpprop:height

rdf:langString 49.62 m

dbpprop:manufacturer

rdf:langString Von Braun

dbpprop:mass

<kilogram> 524484.0

dbpprop:status

rdf:langString Never flown

dbpprop:stages

xsd:integer 3

dbpedia-owl:abstract

rdf:langString 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.

dbpprop:altDiameter

<foot> 21.39

dbpprop:altHeight

<foot> 162.29

dbpprop:countryOrigin

rdf:langString United States

dbpprop:function

rdf:langString Uncrewed launch vehicle

<http://dbpedia.org/ontology/MeanOfTransportation/diameter>

<metre> 6.52

<http://dbpedia.org/ontology/MeanOfTransportation/height>

<millimetre> 49620.0