About: Saturn INT-20

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The Saturn INT-20 was a proposed intermediate-payload follow-on from the Apollo Saturn V launch vehicle. A conical-form interstage would be fitted on top of the S-IC stage to support the S-IVB stage, so it could be considered either a retrofitted Saturn IB with a more powerful first stage, or a stubby, cut-down Saturn V without the S-II second stage. Three variants were studied, one with three F-1 engines in the first stage, one with four, and one with five.

Attributes	Values
rdf:type	Thing mean of transportation Rocket rocket yago:WikicatCancelledSpaceLaunchVehicles yago:Artifact100021939 yago:Conveyance103100490 yago:Instrumentality103575240 yago:Object100002684 yago:PhysicalEntity100001930 yago:Rocket104099429 yago:Vehicle104524313 yago:Whole100003553
rdfs:label	Saturn INT-20 (fr) Saturn INT-20 (pl) Saturn INT-20 (en)
rdfs:comment	Saturn INT-20 a été une proposition de lanceur dérivé de Saturn V. Un inter-étage serait aménagé au-dessus de l'étage S-IC pour soutenir l'étage S-IVB, de sorte qu'il pouvait être considéré soit comme un Saturn IB avec un premier étage plus puissant, soit comme un Saturn V tronqué, sans le deuxième étage S-II. Trois variantes ont été étudiées, l'une avec trois moteurs F-1 dans le premier étage, une à quatre moteurs, et une autre à cinq. (fr) The Saturn INT-20 was a proposed intermediate-payload follow-on from the Apollo Saturn V launch vehicle. A conical-form interstage would be fitted on top of the S-IC stage to support the S-IVB stage, so it could be considered either a retrofitted Saturn IB with a more powerful first stage, or a stubby, cut-down Saturn V without the S-II second stage. Three variants were studied, one with three F-1 engines in the first stage, one with four, and one with five. (en) Saturn INT-20 – rakieta nośna projektowana przez NASA w latach 60. XX wieku o konstrukcji zapożyczonej z rakiety Saturn V. Miała się składać ze stopni S-IC i S-IVB, w związku z czym mogła wyprzeć rakietę Saturn IB. Projekt nie został zrealizowany. (pl)
foaf:name	Saturn INT-20 (en)
name	Saturn INT-20 (en)
foaf:depiction
dcterms:subject	Apollo program Saturn (rocket family) Cancelled space launch vehicles
Wikipage page ID	5882940 (xsd:integer)
Wikipage revision ID	1084022912 (xsd:integer)
Link from a Wikipage to another Wikipage	Rocketdyne F-1 Rocketdyne J-2 Saturn C-3 Saturn IB Saturn V Boeing LH2 S-IC S-II S-IVB Apollo program Launch vehicle Liquid oxygen Saturn (rocket family) Cancelled space launch vehicles Kennedy Space Center Kennedy Space Center Launch Complex 39 Douglas Aircraft Company Space Launch System Nautical mile New Glenn RP-1 LOX Low Earth orbit Rocketdyne Project Apollo F-1 (rocket engine)
Link from a Wikipage to an external page	https://web.archive.org/web/20020829021004/http:/astronautix.com/lvs/satint20.htm https://web.archive.org/web/20060614175128/http:/astronautix.com/data/satvint.pdf
sameAs	Saturn INT-20 Saturn INT-20 Saturn INT-20 Saturn INT-20 Saturn INT-20 Saturn INT-20 Saturn INT-20
sites	Kennedy Space Center Kennedy Space Center Launch Complex 39
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Cvt dbt:Refbegin dbt:Refend dbt:Reflist dbt:Infobox_rocket/stage dbt:Infobox_rocket/payload dbt:Infobox_rocket dbt:Saturns
thumbnail	wiki-commons:Special:FilePath/INT20C.svg?width=300
manufacturer	Boeing Douglas (en)
status	Proposal (en)
stages	2 (xsd:integer)
has abstract	Saturn INT-20 a été une proposition de lanceur dérivé de Saturn V. Un inter-étage serait aménagé au-dessus de l'étage S-IC pour soutenir l'étage S-IVB, de sorte qu'il pouvait être considéré soit comme un Saturn IB avec un premier étage plus puissant, soit comme un Saturn V tronqué, sans le deuxième étage S-II. Trois variantes ont été étudiées, l'une avec trois moteurs F-1 dans le premier étage, une à quatre moteurs, et une autre à cinq. (fr) The Saturn INT-20 was a proposed intermediate-payload follow-on from the Apollo Saturn V launch vehicle. A conical-form interstage would be fitted on top of the S-IC stage to support the S-IVB stage, so it could be considered either a retrofitted Saturn IB with a more powerful first stage, or a stubby, cut-down Saturn V without the S-II second stage. Three variants were studied, one with three F-1 engines in the first stage, one with four, and one with five. (en) Saturn INT-20 – rakieta nośna projektowana przez NASA w latach 60. XX wieku o konstrukcji zapożyczonej z rakiety Saturn V. Miała się składać ze stopni S-IC i S-IVB, w związku z czym mogła wyprzeć rakietę Saturn IB. Projekt nie został zrealizowany. (pl)
country-origin	United States (en)
function	Manned LEO launch vehicle (en)
launch site	Kennedy Space Center Kennedy Space Center Launch Complex 39
rocket function	Low Earth orbit
prov:wasDerivedFrom	wikipedia-en:Saturn_INT-20?oldid=1084022912&ns=0
page length (characters) of wiki page	4563 (xsd:nonNegativeInteger)
status	Proposal
number of rocket stages	2 (xsd:nonNegativeInteger)
manufacturer	Boeing Douglas Aircraft Company
foaf:isPrimaryTopicOf	wikipedia-en:Saturn_INT-20
is Link from a Wikipage to another Wikipage of	Project Gemini Saturn C-3 Saturn II Saturn V List of canceled launch vehicle designs Big Gemini

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