About: Soyuz/Vostok

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

About: Soyuz/Vostok Goto Sponge NotDistinct Permalink

An Entity of Type : yago:Whole100003553, within Data Space : dbpedia.org:8891 associated with source document(s)
QRcode icon

http://dbpedia.org:8891/describe/?url=http%3A%2F%2Fdbpedia.org%2Fresource%2FSoyuz%2FVostok

The Soyuz/Vostok, also known as just Soyuz or Vostok, or by its GRAU index, 11A510 was an interim expendable carrier rocket used by the Soviet Union in 1965 and 1966. Two were launched with prototype US-A satellites.

Attributes	Values
rdf:type	Thing mean of transportation Rocket rocket yago:WikicatSpaceLaunchVehiclesOfTheSovietUnion yago:Artifact100021939 yago:Conveyance103100490 yago:Instrumentality103575240 yago:Object100002684 yago:PhysicalEntity100001930 yago:Rocket104099429 yago:Vehicle104524313 yago:Whole100003553
rdfs:label	Soyuz/Vostok (en) Soyuz/Vostok (in) Soyouz/Vostok (fr) Sojuz-Wostok (pl) Soyuz/Vostok (foguete) (pt)
rdfs:comment	Sojuz-Wostok (ozn. kodowe 11A510) – radziecka rakieta nośna, pochodna pocisku balistycznego R-7. Wykorzystywała ona główne i pomocnicze silniki rakiety Sojuz, drugi człon rakiety Wostok-2 oraz bliżej nieokreślony trzeci stopień. Rakieta powstała wskutek anulowania programu rakiet , w celu wynoszenia prototypowych satelitów RORSAT, do czasu rozpoczęcia eksploatacji rakiety Cyklon-2. (pl) Soyuz/Vostok, juga dikenal sebagai hanya Soyuz atau Vostok, atau dengan indeks Grau nya 11A510 adalah roket pembawa expendable (sekali pakai) interim yang digunakan oleh Uni Soviet pada tahun 1965 dan 1966. Dua diluncurkan dengan prototipe satelit US-A. (in) The Soyuz/Vostok, also known as just Soyuz or Vostok, or by its GRAU index, 11A510 was an interim expendable carrier rocket used by the Soviet Union in 1965 and 1966. Two were launched with prototype US-A satellites. (en) Soyouz/Vostok (indice GRAU : 11A510) était un lanceur soviétique orbital provisoire conçu pour lancer des prototypes de satellites RORSAT en 1965 et 1966. Comme pour le lanceur Polyot, le développement de Soyouz/Vostok est devenu nécessaire pour combler le délai entre l'annulation du programme UR-200 et le lancement de Tsiklon-2 qui a repris les lancements des RORSAT. Soyouz/Vostok était composé de l'étage central et des quatre propulseurs d'une fusée Soyouz combinés au deuxième étage de (en) et d'un étage supérieur développé pour le futur Tsiklon, faisant partie de la charge utile. (fr) O foguete Soyuz/Vostok (11A510), foi um veículo de lançamento descartável, usado pela União Soviética entre 1965 e 1966. Este modelo tinha uma finalidade específica, e efetuou apenas dois lançamentos. Ele foi originalmente projetado como uma versão especializada dentro da família de foguetes Vostok, para lançar os protótipos dos satélites RORSAT devido ao cancelamento do projeto UR-200, que seria o seu lançador "oficial". Assim como o foguete Polyot, este modelo foi um desenvolvimento intermediário entre o cancelamento do projeto UR-200, e o desenvolvimento do foguete Tsyklon-2. (pt)
foaf:name	Soyuz/Vostok (en)
name	Soyuz/Vostok (en)
dcterms:subject	Space launch vehicles of the Soviet Union Vehicles introduced in 1965 R-7 (rocket family)
Wikipage page ID	22423008 (xsd:integer)
Wikipage revision ID	1092540208 (xsd:integer)
Link from a Wikipage to another Wikipage	Space launch vehicles of the Soviet Union Voskhod (rocket) Vostok-2 (rocket) Vehicles introduced in 1965 R-7 (rocket family) RD-108 R-7 (rocket family) Baikonur Cosmodrome Baikonur Cosmodrome Site 31 Tsyklon-2 UR-200 Launch vehicle OKB-1 Polyot (rocket) Soviet Union Soyuz (rocket) RD-0109 RD-107 RP-1 Expendable launch system LOX Low Earth orbit RORSAT GRAU index
sameAs	Soyuz/Vostok Soyuz/Vostok Soyuz/Vostok Soyuz/Vostok Soyuz/Vostok Soyuz/Vostok Soyuz/Vostok Soyuz/Vostok Soyuz/Vostok
sites	Baikonur Cosmodrome Baikonur Cosmodrome Site 31
dbp:wikiPageUsesTemplate	dbt:R-7_rockets dbt:Expendable_launch_systems dbt:No_orbit_for_payload dbt:Infobox_Rocket dbt:Convert dbt:Refimprove dbt:Reflist dbt:Russian_launch_vehicles dbt:Infobox_Rocket/Payload dbt:Infobox_Rocket/Stage
success	2 (xsd:integer)
family	R-7 (rocket family)
first	1965-12-27 (xsd:date)
last	1966-07-20 (xsd:date)
manufacturer	OKB-1
status	Retired (en)
stages	Three (en)
has abstract	Soyouz/Vostok (indice GRAU : 11A510) était un lanceur soviétique orbital provisoire conçu pour lancer des prototypes de satellites RORSAT en 1965 et 1966. Comme pour le lanceur Polyot, le développement de Soyouz/Vostok est devenu nécessaire pour combler le délai entre l'annulation du programme UR-200 et le lancement de Tsiklon-2 qui a repris les lancements des RORSAT. Soyouz/Vostok était composé de l'étage central et des quatre propulseurs d'une fusée Soyouz combinés au deuxième étage de (en) et d'un étage supérieur développé pour le futur Tsiklon, faisant partie de la charge utile. C'est un membre de la famille R-7. (fr) Soyuz/Vostok, juga dikenal sebagai hanya Soyuz atau Vostok, atau dengan indeks Grau nya 11A510 adalah roket pembawa expendable (sekali pakai) interim yang digunakan oleh Uni Soviet pada tahun 1965 dan 1966. Dua diluncurkan dengan prototipe satelit US-A. Soyuz / Vostok diluncurkan dari Site 31/6 di Kosmodrom Baikonur. Ini terdiri dari tahap pertama dan penguat dari roket Soyuz dikombinasikan dengan tahap kedua Vostok-2, dan tahap ketiga yang tidak diketahui.Seiring dengan Polyot Voskhod yang diturunkan, itu dibangun sebagai interim antara pembatalan program pengembangan UR-200, dan pengenalan Tsyklon-2, yang mengambil alih peluncurkan US-A setelah memasuki layanan. (in) The Soyuz/Vostok, also known as just Soyuz or Vostok, or by its GRAU index, 11A510 was an interim expendable carrier rocket used by the Soviet Union in 1965 and 1966. Two were launched with prototype US-A satellites. The Soyuz/Vostok was launched from Site 31/6 at the Baikonur Cosmodrome. It consisted of the first stage and boosters from a Soyuz rocket combined with the second stage of the Vostok-2, and an unknown third stage. Along with the Voskhod-derived Polyot, it was built as an interim between the cancellation of the UR-200 development programme, and the introduction of the Tsyklon-2, which took over US-A launches once it entered service. (en) Sojuz-Wostok (ozn. kodowe 11A510) – radziecka rakieta nośna, pochodna pocisku balistycznego R-7. Wykorzystywała ona główne i pomocnicze silniki rakiety Sojuz, drugi człon rakiety Wostok-2 oraz bliżej nieokreślony trzeci stopień. Rakieta powstała wskutek anulowania programu rakiet , w celu wynoszenia prototypowych satelitów RORSAT, do czasu rozpoczęcia eksploatacji rakiety Cyklon-2. (pl) O foguete Soyuz/Vostok (11A510), foi um veículo de lançamento descartável, usado pela União Soviética entre 1965 e 1966. Este modelo tinha uma finalidade específica, e efetuou apenas dois lançamentos. Ele foi originalmente projetado como uma versão especializada dentro da família de foguetes Vostok, para lançar os protótipos dos satélites RORSAT devido ao cancelamento do projeto UR-200, que seria o seu lançador "oficial". Assim como o foguete Polyot, este modelo foi um desenvolvimento intermediário entre o cancelamento do projeto UR-200, e o desenvolvimento do foguete Tsyklon-2. Era um foguete de três estágios, sendo: * O primeiro estágio e os foguetes auxiliares do Soyuz, * O segundo estágio do Vostok 2, * O terceiro estágio, foram testes com o que viria a ser o estágio superior do Tsyklon-2. (pt)
country-origin	Soviet Union
function	Interim carrier rocket (en)
launches	2 (xsd:integer)
payloads	RORSAT
country origin	Soviet Union
launch site	Baikonur Cosmodrome
gold:hypernym	Rocket
final flight	1966-07-20 (xsd:date)
maiden flight	1965-12-27 (xsd:date)
prov:wasDerivedFrom	wikipedia-en:Soyuz/Vostok?oldid=1092540208&ns=0
page length (characters) of wiki page	3013 (xsd:nonNegativeInteger)
status	Retired
successful launches	2 (xsd:nonNegativeInteger)

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 08.03.3331 as of Sep 2 2024, on Linux (x86_64-generic-linux-glibc212), Single-Server Edition (62 GB total memory, 43 GB memory in use)
Data on this page belongs to its respective rights holders.
Virtuoso Faceted Browser Copyright © 2009-2024 OpenLink Software