| dbo:MeanOfTransportation/diameter
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| dbo:MeanOfTransportation/height
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| dbo:MeanOfTransportation/mass
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| dbo:Rocket/mass
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| dbo:abstract
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- El Saturno C-2 fue el cohete inicialmente considerado (en 1960) para llevar a cabo el primer alunizaje tripulado del programa Apolo. No pasó de la fase de estudio. Mucho menos potente que el futuro Saturno V, se habrían necesitado 15 lanzamientos de cohetes Saturno C-2 para montar una nave en órbita baja terrestre capaz de viajar hasta la Luna y aterrizar en ella. (es)
- The Saturn C-2 was the second rocket in the Saturn C series studied from 1959 to 1962. The design was for a four-stage launch vehicle that could launch 21,500 kg (47,300 lb) to low Earth orbit and send 6,800 kg (14,900 lb) to the Moon via Trans-Lunar Injection.The C-2 design concept was for a proposed crewed circumlunar flight and the Earth orbit rendezvous (EOR) missions. It was initially considered for the Apollo lunar landing at the earliest possible date (1967). (en)
- Il Saturn C-2 era un prototipo di un veicolo di lancio statunitense, progettato per realizzare lo scenario di Earth Orbit Rendezvous per le missioni spaziali verso la Luna del Programma Apollo. Il progetto era stato studiato prima nel 1960, ed era stato calcolato che sarebbero necessari 15 lanci per assemblare il veicolo spaziale in orbita bassa terrestre. (it)
- Saturn C-2 en raket i Saturn-serien som aldrig kom längre än ritbordet. (sv)
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| dbo:diameter
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| dbo:height
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| dbo:launchSite
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| dbo:mass
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- 620071200.000000 (xsd:double)
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| dbo:rocketFunction
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| dbo:status
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| dbo:wikiPageExternalLink
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| dbo:wikiPageID
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| dbo:wikiPageLength
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- 9628 (xsd:nonNegativeInteger)
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| dbo:wikiPageRevisionID
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| dbo:wikiPageWikiLink
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| dbp:countryOrigin
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| dbp:family
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| dbp:function
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- Launch vehicle for Project Horizon and Apollo (en)
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| dbp:mass
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| dbp:sites
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| dbp:status
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- Study, not developed (en)
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| dbp:wikiPageUsesTemplate
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| dcterms:subject
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| gold:hypernym
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| rdf:type
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| rdfs:comment
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- El Saturno C-2 fue el cohete inicialmente considerado (en 1960) para llevar a cabo el primer alunizaje tripulado del programa Apolo. No pasó de la fase de estudio. Mucho menos potente que el futuro Saturno V, se habrían necesitado 15 lanzamientos de cohetes Saturno C-2 para montar una nave en órbita baja terrestre capaz de viajar hasta la Luna y aterrizar en ella. (es)
- The Saturn C-2 was the second rocket in the Saturn C series studied from 1959 to 1962. The design was for a four-stage launch vehicle that could launch 21,500 kg (47,300 lb) to low Earth orbit and send 6,800 kg (14,900 lb) to the Moon via Trans-Lunar Injection.The C-2 design concept was for a proposed crewed circumlunar flight and the Earth orbit rendezvous (EOR) missions. It was initially considered for the Apollo lunar landing at the earliest possible date (1967). (en)
- Il Saturn C-2 era un prototipo di un veicolo di lancio statunitense, progettato per realizzare lo scenario di Earth Orbit Rendezvous per le missioni spaziali verso la Luna del Programma Apollo. Il progetto era stato studiato prima nel 1960, ed era stato calcolato che sarebbero necessari 15 lanci per assemblare il veicolo spaziale in orbita bassa terrestre. (it)
- Saturn C-2 en raket i Saturn-serien som aldrig kom längre än ritbordet. (sv)
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| rdfs:label
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- Saturno C-2 (es)
- Saturn C-2 (it)
- Saturn C-2 (en)
- Saturn C-2 (sv)
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| prov:wasDerivedFrom
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| foaf:isPrimaryTopicOf
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| is dbo:wikiPageWikiLink
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| is dbp:rockets
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| is foaf:primaryTopic
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