The RD-263 (GRAU Index 15D117) is a liquid rocket engine, burning N2O4 and UDMH in the oxidizer rich staged combustion cycle. Four RD-263 engines form a propulsion module RD-264 (GRAU Index 15D119). For the R-36M KB Yuzhnoye only ordered the first stage propulsion to Energomash, instead of both stages, arguing that they were overworked with the RD-270 development. By April 1970 Yuzhnoye was getting the engine documentation. By the end of 1972 Energomash started to test fire the engines in its own test stand. And by September 1973 the engine was certified for flight. While the engine is out of production, the ICBM as well as the Dnepr remain operational as of 2015.
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| - RD-263 (fr)
- RD-263 (ko)
- RD-263 (ja)
- RD-263 (en)
- RD-263 (pt)
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| - The RD-263 (GRAU Index 15D117) is a liquid rocket engine, burning N2O4 and UDMH in the oxidizer rich staged combustion cycle. Four RD-263 engines form a propulsion module RD-264 (GRAU Index 15D119). For the R-36M KB Yuzhnoye only ordered the first stage propulsion to Energomash, instead of both stages, arguing that they were overworked with the RD-270 development. By April 1970 Yuzhnoye was getting the engine documentation. By the end of 1972 Energomash started to test fire the engines in its own test stand. And by September 1973 the engine was certified for flight. While the engine is out of production, the ICBM as well as the Dnepr remain operational as of 2015. (en)
- Le RD-263 (indice GRAU 15D117) est un moteur-fusée à ergols liquides, brûlant du N2O4 et de l'UDMH selon le cycle à combustion étagée riche en oxydant. Quatre moteurs RD-263 forment un module de propulsion RD-264 (indice GRAU 15D119). Pour le missile R-36M, KB Ioujnoïe commanda seulement la propulsion du premier étage à Energomach, au lieu des deux étages, prétextant qu'ils étaient surchargés par le développement du RD-270. En avril 1970, Ioujnoïe a reçu la documentation du moteur. Fin 1972, Energomash commença les tests de mise à feu des moteurs sur son banc d'essais. Et en septembre 1973, le moteur fut certifié pour le vol. Bien que le moteur ne soit plus en production, le missile R-36 et la fusée Dnepr restent opérationnels en 2015. (fr)
- RD-263은 러시아의 액체연료 로켓 엔진이다. (ko)
- RD-263 (GRAU 分類 15D117) はN2O4とUDMHを酸化剤リッチ二段燃焼サイクルで燃焼する液体 ロケットエンジンであるRD-264 (GRAU 分類 15D119)推進モジュールは4基の RD-263 である。 R-36M KB ユージュノエのみが1段目の推進をエネゴマシュへ発注し、両段の代わりにRD-270が開発された。1970年4月にユージュノエはエンジンの書類を入手した。1972年末以降エネゴマシュは独自の試験設備でエンジンの燃焼試験を開始した。1973年9月にエンジンは飛行のための認証を取得した。 エンジンの製造は終了したものの、ICBM と同様に2015年時点でドニエプル-1が運用中である。 (ja)
- O RD-263 (ou 15D117) é um motor de foguete de combustível líquido desenvolvido na União Soviética na Energomash queimando N2O4 e UDMH, em um ciclo de combustão em estágios. Quatro motores RD-263 agrupados, formam o módulo de propulsão RD-264 (ou 15D119). para o míssil R-36M. A KB Yuzhnoye só encomendou a propulsão para o primeiro estágio, argumentando que a Energomash, estava sobrecarregada com o desenvolvimento do RD-270. Em meados de abril de 1970, a Yuzhnoye recebia a documentação do motor. No final de 1972 a Energomash iniciou os testes de ignição do motor no seu próprio estande de testes. Em setembro de 1973 o motor estava certificado para voos. Apesar desse motor ter saído de linha, o míssil R-36 assim como o foguete Dnepr continuaram operacionais até ao menos 2015.O RD-263 gera um e (pt)
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| - R-36M and R-36MUTTKh core stage (en)
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| - The RD-263 (GRAU Index 15D117) is a liquid rocket engine, burning N2O4 and UDMH in the oxidizer rich staged combustion cycle. Four RD-263 engines form a propulsion module RD-264 (GRAU Index 15D119). For the R-36M KB Yuzhnoye only ordered the first stage propulsion to Energomash, instead of both stages, arguing that they were overworked with the RD-270 development. By April 1970 Yuzhnoye was getting the engine documentation. By the end of 1972 Energomash started to test fire the engines in its own test stand. And by September 1973 the engine was certified for flight. While the engine is out of production, the ICBM as well as the Dnepr remain operational as of 2015. (en)
- Le RD-263 (indice GRAU 15D117) est un moteur-fusée à ergols liquides, brûlant du N2O4 et de l'UDMH selon le cycle à combustion étagée riche en oxydant. Quatre moteurs RD-263 forment un module de propulsion RD-264 (indice GRAU 15D119). Pour le missile R-36M, KB Ioujnoïe commanda seulement la propulsion du premier étage à Energomach, au lieu des deux étages, prétextant qu'ils étaient surchargés par le développement du RD-270. En avril 1970, Ioujnoïe a reçu la documentation du moteur. Fin 1972, Energomash commença les tests de mise à feu des moteurs sur son banc d'essais. Et en septembre 1973, le moteur fut certifié pour le vol. Bien que le moteur ne soit plus en production, le missile R-36 et la fusée Dnepr restent opérationnels en 2015. (fr)
- RD-263은 러시아의 액체연료 로켓 엔진이다. (ko)
- RD-263 (GRAU 分類 15D117) はN2O4とUDMHを酸化剤リッチ二段燃焼サイクルで燃焼する液体 ロケットエンジンであるRD-264 (GRAU 分類 15D119)推進モジュールは4基の RD-263 である。 R-36M KB ユージュノエのみが1段目の推進をエネゴマシュへ発注し、両段の代わりにRD-270が開発された。1970年4月にユージュノエはエンジンの書類を入手した。1972年末以降エネゴマシュは独自の試験設備でエンジンの燃焼試験を開始した。1973年9月にエンジンは飛行のための認証を取得した。 エンジンの製造は終了したものの、ICBM と同様に2015年時点でドニエプル-1が運用中である。 (ja)
- O RD-263 (ou 15D117) é um motor de foguete de combustível líquido desenvolvido na União Soviética na Energomash queimando N2O4 e UDMH, em um ciclo de combustão em estágios. Quatro motores RD-263 agrupados, formam o módulo de propulsão RD-264 (ou 15D119). para o míssil R-36M. A KB Yuzhnoye só encomendou a propulsão para o primeiro estágio, argumentando que a Energomash, estava sobrecarregada com o desenvolvimento do RD-270. Em meados de abril de 1970, a Yuzhnoye recebia a documentação do motor. No final de 1972 a Energomash iniciou os testes de ignição do motor no seu próprio estande de testes. Em setembro de 1973 o motor estava certificado para voos. Apesar desse motor ter saído de linha, o míssil R-36 assim como o foguete Dnepr continuaram operacionais até ao menos 2015.O RD-263 gera um empuxo de 1.040 kN, isp de 293 s, pressão na câmara de 20,6 MPa com 2,15 m de comprimento e 1 m de diâmetro, pesa 870 kg. (pt)
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