The RD-864 (GRAU: 15D177) is a Soviet liquid propellant rocket engine burning UDMH and nitrogen tetroxide in a gas generator combustion cycle. It has a four combustion chambers that provide thrust vector control by gimbaling each nozzle in a single axis ±55°. It is used on the third stage of the R-36M UTTKh (GRAU: 15A18) and Dnepr. For the R-36M2 (GRAU: 15A18M), an improved version, the RD-869 (GRAU: 15D300) was developed.
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| - RD-864 (fr)
- RD-864 (en)
- RD-864 (pt)
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| - The RD-864 (GRAU: 15D177) is a Soviet liquid propellant rocket engine burning UDMH and nitrogen tetroxide in a gas generator combustion cycle. It has a four combustion chambers that provide thrust vector control by gimbaling each nozzle in a single axis ±55°. It is used on the third stage of the R-36M UTTKh (GRAU: 15A18) and Dnepr. For the R-36M2 (GRAU: 15A18M), an improved version, the RD-869 (GRAU: 15D300) was developed. (en)
- Le RD-864 (indice GRAU : 15D177) est un moteur-fusée à ergols liquides soviétique brûlant de l'UDMH et du peroxyde d'azote selon un cycle de combustion générateur de gaz. Il possède quatre chambres de combustion qui fournissent un contrôle du vecteur de poussée en inclinant chacune des tuyères selon un seul axe à ±55°. Il est utilisé sur le troisième étage du missile R-36M UTTKh (indice GRAU : 15A18) et de la fusée Dnepr. Pour le missile R-36M2 (indice GRAU : 15A18M), une version améliorée, le RD-869 (indice GRAU : 15D300) a été développée. (fr)
- O RD-864 (GRAU: 15D177) é um motor soviético de foguete de combustível líquido que queimava UDMH e N2O4 num ciclo gerador de gás. Ele possui quatro câmaras de combustão exercendo a função de controle de atitude movimentando cada bocal num único eixo de +/- 55°. Ele é usado no terceiro estágio do R-36M UTTKh (GRAU: 15A18) e do Dnepr. Para o R-36M2 (GRAU: 15A18M), uma versão melhorada, a RD-869 (GRAU: 15D300) foi desenvolvida. (pt)
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| - Upper stage (en)
- Upper Stage (en)
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| - R-36M UTTKh and Dnepr third stage (en)
- R-36M2 third stage (en)
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| - The RD-864 (GRAU: 15D177) is a Soviet liquid propellant rocket engine burning UDMH and nitrogen tetroxide in a gas generator combustion cycle. It has a four combustion chambers that provide thrust vector control by gimbaling each nozzle in a single axis ±55°. It is used on the third stage of the R-36M UTTKh (GRAU: 15A18) and Dnepr. For the R-36M2 (GRAU: 15A18M), an improved version, the RD-869 (GRAU: 15D300) was developed. (en)
- Le RD-864 (indice GRAU : 15D177) est un moteur-fusée à ergols liquides soviétique brûlant de l'UDMH et du peroxyde d'azote selon un cycle de combustion générateur de gaz. Il possède quatre chambres de combustion qui fournissent un contrôle du vecteur de poussée en inclinant chacune des tuyères selon un seul axe à ±55°. Il est utilisé sur le troisième étage du missile R-36M UTTKh (indice GRAU : 15A18) et de la fusée Dnepr. Pour le missile R-36M2 (indice GRAU : 15A18M), une version améliorée, le RD-869 (indice GRAU : 15D300) a été développée. (fr)
- O RD-864 (GRAU: 15D177) é um motor soviético de foguete de combustível líquido que queimava UDMH e N2O4 num ciclo gerador de gás. Ele possui quatro câmaras de combustão exercendo a função de controle de atitude movimentando cada bocal num único eixo de +/- 55°. Ele é usado no terceiro estágio do R-36M UTTKh (GRAU: 15A18) e do Dnepr. Para o R-36M2 (GRAU: 15A18M), uma versão melhorada, a RD-869 (GRAU: 15D300) foi desenvolvida. (pt)
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| - R-36M
- R-36M UTTKh and Dnepr (en)
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