About: Saturn C-3

Facets (new session)
Description
Metadata
Settings
- Rule:
- Inverse Functional Properties:
- "Same As":

About: Saturn C-3 Goto Sponge NotDistinct Permalink

An Entity of Type : yago:Whole100003553, within Data Space : dbpedia.demo.openlinksw.com associated with source document(s)
QRcode icon

http://dbpedia.demo.openlinksw.com/describe/?url=http%3A%2F%2Fdbpedia.org%2Fresource%2FSaturn_C-3

The Saturn C-3 was the third rocket in the Saturn C series studied from 1959 to 1962. The design was for a three-stage launch vehicle that could launch 45,000 kilograms (99,000 lb) to low Earth orbit and send 18,000 kilograms (40,000 lb) to the Moon via trans-lunar injection. This decision ended consideration of a Nova class launch vehicle for a direct ascent to the Moon or as a heavy-lift companion with the Saturn C-3 for Earth orbit rendezvous.

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	ساتورن سي 3 (ar) Saturn C-3 (en) Saturno C-3 (es) Saturn C-3 (fr) Saturn C-3 (it)
rdfs:comment	El Saturno C-3 fue uno de los cohetes inicialmente considerados (en 1960) para llevar a cabo el primer alunizaje tripulado del programa Apolo. No pasó de la fase de estudio. Fue pensado para poner en práctica el esquema de "cita en órbita terrestre", en el que se realizaban varios lanzamientos para montar en órbita baja terrestre las naves que luego viajarían hasta la Luna. (es) Il Saturn C-3 è stato il terzo razzo della serie Saturn C, studiato nel 1960. Il Saturn C-3 è stato destinato ad essere utilizzato per lo scenario dell'Earth Orbit Rendezvous nell'ambito del Programma Apollo. Il lanciatore consisteva in un primo stadio dotato di due motori F-1, un secondo stadio con quattro potenti motori J-2 e lo stadio S-IV di un Saturn I. Tutti gli stadi del Saturn C-3, ad eccezione del S-IV, non hanno mai volato se non per i loro motori, utilizzati sul razzo Saturn V che ha portato gli uomini sulla Luna. (it) كان صاروخ ساتورن سي 3 الصاروخ الثالث في سلسلة صواريخ ساتورن سي التي دُرست بين عامي 1959 و1962. شمل التصميم مركبة إطلاق ثلاثية المراحل يمكنها حمل 45000 كيلوغرام (99000 باوند) إلى مدار أرضي منخفض وإرسال 18000 كيلوغرام (40000 باوند) إلى القمر عن طريق الدخول في مدار انتقالي قمري. أنهى هذا القرار العمل على صواريخ فئة نوفا لاستخدامها للصعود المباشر إلى القمر أو كمركبة رفع ثقيل مرافقة لصاروخ ساتورن سي 3 لالتقاء الأرضي المداري. (ar) The Saturn C-3 was the third rocket in the Saturn C series studied from 1959 to 1962. The design was for a three-stage launch vehicle that could launch 45,000 kilograms (99,000 lb) to low Earth orbit and send 18,000 kilograms (40,000 lb) to the Moon via trans-lunar injection. This decision ended consideration of a Nova class launch vehicle for a direct ascent to the Moon or as a heavy-lift companion with the Saturn C-3 for Earth orbit rendezvous. (en) La Saturn C-3 était la troisième fusée de la série Saturn C étudiée de 1959 à 1962. La conception était pour un lanceur à trois étages qui pourrait lancer 45 t en orbite terrestre basse et envoyer 18 t vers la Lune par injection trans-lunaire . Cette décision a mis fin à l'examen d'un lanceur de classe Nova pour une ascension directe vers la Lune ou comme compagnon de transport lourd avec le Saturn C-3 pour le rendez-vous en orbite terrestre. (fr)
foaf:name	Saturn C-3 (en)
name	Saturn C-3 (en)
foaf:depiction
dcterms:subject	Apollo program Saturn (rocket family) Cancelled space launch vehicles
Wikipage page ID	11083533 (xsd:integer)
Wikipage revision ID	1110298903 (xsd:integer)
Link from a Wikipage to another Wikipage	Cape Canaveral Air Force Station Space Launch Complex 37 Project Gemini Rocket Rocketdyne F-1 Saturn C-4 Saturn C-8 Saturn I Saturn IB Saturn INT-20 Saturn INT-21 Saturn V Boeing Delta IV Delta IV Heavy Earth orbit rendezvous Orbit LH2 Common Booster Core S-IB S-IC S-II S-IV Nova (rocket) Moon NERVA Apollo program Lunar orbit rendezvous Apollo program Trans-lunar injection Trans Lunar Injection Vulcan (rocket) Launch vehicle Liquid oxygen Geostationary Transfer Orbit Agena target vehicle Earth Falcon Heavy North American Aviation Spacecraft Jarvis (rocket) Saturn (rocket family) Advanced Launch System Cancelled space launch vehicles John Houbolt Kennedy Space Center Douglas Aircraft Company Space Launch System Space Shuttle Challenger disaster Space Shuttle external tank Michoud Assembly Facility New Glenn RL10 RP-1 Saturn (rocket family) LOX Low Earth orbit Rocketdyne Saturn rocket J-2 (rocket engine) SLC 37 F-1 (rocket engine) dbr:S-IB-2 dbr:S-II-C3

Faceted Search & Find service v1.17_git139 as of Feb 29 2024

Alternative Linked Data Documents: ODE Content Formats:

RDF

ODATA

Microdata

About

OpenLink Virtuoso version 08.03.3330 as of Mar 19 2024, on Linux (x86_64-generic-linux-glibc212), Single-Server Edition (378 GB total memory, 59 GB memory in use)
Data on this page belongs to its respective rights holders.
Virtuoso Faceted Browser Copyright © 2009-2024 OpenLink Software