RD-215 (original) (raw)
The RD-215 (GRAU Index 8D513) was a dual nozzle liquid rocket engine, burning AK-27 (a mixture of 73% nitric acid and 27% N2O4 + iodine passivant) and UDMH. It was used in a module of two engines (four nozzles) known as the RD-216 (GRAU Index 8D514). The RD-215 was developed by OKB-456 for Yangel's Yuzhmash R-14 (8K65) ballistic missile. Its variations were also used on the Kosmos-1, Kosmos-3 and Kosmos-3M launch vehicles.
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| dbo:abstract | The RD-215 (GRAU Index 8D513) was a dual nozzle liquid rocket engine, burning AK-27 (a mixture of 73% nitric acid and 27% N2O4 + iodine passivant) and UDMH. It was used in a module of two engines (four nozzles) known as the RD-216 (GRAU Index 8D514). The RD-215 was developed by OKB-456 for Yangel's Yuzhmash R-14 (8K65) ballistic missile. Its variations were also used on the Kosmos-1, Kosmos-3 and Kosmos-3M launch vehicles. (en) Le RD-215 (indice GRAU 8D513) était un moteur-fusée à ergols liquides à deux tuyères, brûlant du AK-27 (un mélange de 73 % d'acide nitrique et de 27 % de N2O4 + iode comme passivant) et de l'UDMH. Il était utilisé dans un module composé de deux moteurs (quatre tuyères) appelé RD-216 (indice GRAU 8D514). Le RD-215 fut développé par l'OKB-456 pour le R-14 (8K65) de Yanguel (Ioujmach). Des variantes furent aussi utilisées sur les lanceurs Kosmos-1, Kosmos-3 et Kosmos-3M. (fr) O RD-215 (GRAU Index 8D513) foi um motor de foguete de combustível líquido queimando AK-27I (uma mistura de 73% de ácido nítrico e 27% de N2O4 + iodo como passivante) e UDMH. Ele foi usado num módulo de dois motores (quatro bocais), conhecido como RD-216 (GRAU Index 8D514). O RD-215 foi desenvolvido pelo OKB-456 para o projeto do míssil de teatro de operações R-14 (8K65), de Yangel na Yuzhmash. Suas variações foram usadas também nos veículos lançadores Kosmos-1, Kosmos-3 e Kosmos-3M. O RD-215 gera um empuxo de 887 kN, pressão na câmara de 7,3 MPa, Isp de 246 s, comprimento de 2,2 m, diâmetro de 2,2 m e peso vazio de 575 kg. (pt) |
| dbo:thumbnail | wiki-commons:Special:FilePath/RD-216_sheme.svg?width=300 |
| dbo:wikiPageExternalLink | http://www.npoenergomash.ru/ |
| dbo:wikiPageID | 51001785 (xsd:integer) |
| dbo:wikiPageLength | 7745 (xsd:nonNegativeInteger) |
| dbo:wikiPageRevisionID | 1104389392 (xsd:integer) |
| dbo:wikiPageWikiLink | dbr:Unsymmetrical_dimethylhydrazine dbr:Valentin_Glushko dbc:Rocket_engines_of_the_Soviet_Union dbr:GRAU dbr:NPO_Energomash dbr:Yuzhmash dbr:Passivation_(chemistry) dbr:Theatre_ballistic_missile dbr:USSR dbr:Launch_vehicle dbr:Nitric_acid dbr:Iodine dbr:Dinitrogen_tetroxide dbr:Kosmos-1 dbr:Kosmos-3 dbr:Kosmos-3M dbr:Mikhail_Yangel dbr:R-14_Chusovaya dbr:R-16_(missile) dbr:Rocket_engine dbr:Liquid-fuel_rocket |
| dbp:associated | R-14, Kosmos-3 and Kosmos-3M (en) |
| dbp:combustionChamber | 2 (xsd:integer) |
| dbp:countryOfOrigin | dbr:USSR |
| dbp:date | 1958 (xsd:integer) |
| dbp:designer | dbr:Valentin_Glushko dbr:NPO_Energomash |
| dbp:fuel | dbr:Unsymmetrical_dimethylhydrazine |
| dbp:mixtureRatio | 2.500000 (xsd:double) |
| dbp:name | RD-215 (en) |
| dbp:nozzleRatio | 18.800000 (xsd:double) |
| dbp:oxidiser | dbr:Nitric_acid |
| dbp:status | Retired (en) |
| dbp:type | liquid (en) |
| dbp:usedIn | R-14, Kosmos-3 and Kosmos-3M first stage (en) |
| dbp:wikiPageUsesTemplate | dbt:Convert dbt:Infobox_rocket_engine dbt:Portal dbt:Reflist dbt:Rocket_engines dbt:Short_description dbt:Sub |
| dcterms:subject | dbc:Rocket_engines_of_the_Soviet_Union |
| rdfs:comment | The RD-215 (GRAU Index 8D513) was a dual nozzle liquid rocket engine, burning AK-27 (a mixture of 73% nitric acid and 27% N2O4 + iodine passivant) and UDMH. It was used in a module of two engines (four nozzles) known as the RD-216 (GRAU Index 8D514). The RD-215 was developed by OKB-456 for Yangel's Yuzhmash R-14 (8K65) ballistic missile. Its variations were also used on the Kosmos-1, Kosmos-3 and Kosmos-3M launch vehicles. (en) Le RD-215 (indice GRAU 8D513) était un moteur-fusée à ergols liquides à deux tuyères, brûlant du AK-27 (un mélange de 73 % d'acide nitrique et de 27 % de N2O4 + iode comme passivant) et de l'UDMH. Il était utilisé dans un module composé de deux moteurs (quatre tuyères) appelé RD-216 (indice GRAU 8D514). Le RD-215 fut développé par l'OKB-456 pour le R-14 (8K65) de Yanguel (Ioujmach). Des variantes furent aussi utilisées sur les lanceurs Kosmos-1, Kosmos-3 et Kosmos-3M. (fr) O RD-215 (GRAU Index 8D513) foi um motor de foguete de combustível líquido queimando AK-27I (uma mistura de 73% de ácido nítrico e 27% de N2O4 + iodo como passivante) e UDMH. Ele foi usado num módulo de dois motores (quatro bocais), conhecido como RD-216 (GRAU Index 8D514). O RD-215 foi desenvolvido pelo OKB-456 para o projeto do míssil de teatro de operações R-14 (8K65), de Yangel na Yuzhmash. Suas variações foram usadas também nos veículos lançadores Kosmos-1, Kosmos-3 e Kosmos-3M. O RD-215 gera um empuxo de 887 kN, pressão na câmara de 7,3 MPa, Isp de 246 s, comprimento de 2,2 m, diâmetro de 2,2 m e peso vazio de 575 kg. (pt) |
| rdfs:label | RD-215 (fr) RD-215 (en) RD-215 (pt) |
| owl:sameAs | yago-res:RD-215 wikidata:RD-215 dbpedia-fr:RD-215 dbpedia-pt:RD-215 https://global.dbpedia.org/id/2Qz1K |
| prov:wasDerivedFrom | wikipedia-en:RD-215?oldid=1104389392&ns=0 |
| foaf:depiction | wiki-commons:Special:FilePath/RD-216_sheme.svg |
| foaf:homepage | http://www.npoenergomash.ru/ |
| foaf:isPrimaryTopicOf | wikipedia-en:RD-215 |
| is dbo:wikiPageDisambiguates of | dbr:215_(disambiguation) |
| is dbo:wikiPageRedirects of | dbr:RD-216 dbr:RD-217 dbr:RD-218 dbr:RD-219 dbr:RD-215M dbr:RD-215U dbr:RD-216M dbr:RD-216U |
| is dbo:wikiPageWikiLink of | dbr:215_(disambiguation) dbr:R-16_(missile) dbr:RD-216 dbr:RD-217 dbr:RD-218 dbr:RD-219 dbr:RD-215M dbr:RD-215U dbr:RD-216M dbr:RD-216U |
| is foaf:primaryTopic of | wikipedia-en:RD-215 |
