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The RD-215 (GRAU Index 8D513) was a dual n … 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.1, Kosmos-3 and Kosmos-3M launch vehicles.
, Le RD-215 (indice GRAU 8D513) était un mot … 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. lanceurs Kosmos-1, Kosmos-3 et Kosmos-3M.
, O RD-215 (GRAU Index 8D513) foi um motor d … 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. diâmetro de 2,2 m e peso vazio de 575 kg.
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http://www.npoenergomash.ru/ +
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51001785
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7745
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R-14, Kosmos-3 and Kosmos-3M
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2
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http://dbpedia.org/resource/USSR +
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1958
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http://dbpedia.org/resource/Unsymmetrical_dimethylhydrazine +
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2.5
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RD-215
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18.8
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http://dbpedia.org/resource/Nitric_acid +
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Retired
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liquid
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R-14, Kosmos-3 and Kosmos-3M first stage
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| rdfs:comment |
The RD-215 (GRAU Index 8D513) was a dual n … 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.1, Kosmos-3 and Kosmos-3M launch vehicles.
, Le RD-215 (indice GRAU 8D513) était un mot … 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. lanceurs Kosmos-1, Kosmos-3 et Kosmos-3M.
, O RD-215 (GRAU Index 8D513) foi um motor d … 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. diâmetro de 2,2 m e peso vazio de 575 kg.
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| rdfs:label |
RD-215
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