| dbo:abstract |
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) |
| dbo:wikiPageExternalLink |
http://www.yuzhnoye.com/en/home/ |
| dbo:wikiPageID |
51019505 (xsd:integer) |
| dbo:wikiPageLength |
11283 (xsd:nonNegativeInteger) |
| dbo:wikiPageRevisionID |
1100164336 (xsd:integer) |
| dbo:wikiPageWikiLink |
dbr:Ukraine dbr:Unsymmetrical_dimethylhydrazine dbr:Intercontinental_ballistic_missile dbc:Rocket_engines_of_the_Soviet_Union dbc:Rocket_engines_using_hypergolic_propellant dbr:START_I dbr:START_II dbr:GRAU dbc:Rocket_engines_of_Ukraine dbr:Yuzhmash dbr:Gas-generator_cycle_(rocket) dbc:Rocket_engines_using_the_gas-generator_cycle dbr:Gimbaled_thrust dbr:Launch_vehicle dbc:Yuzhmash_rocket_engines dbc:Yuzhnoye_rocket_engines dbr:Dinitrogen_tetroxide dbr:Dnepr_(rocket) dbr:Soviet_Union dbr:R-36M dbr:Mikhail_Yangel dbr:Thrust_vectoring dbr:Yuzhnoye_Design_Bureau dbr:UDMH dbr:Liquid-fuel_rocket dbr:RD-869 dbr:Yuzhnoe_Design_Bureau |
| dbp:associated |
dbr:R-36M R-36M UTTKh and Dnepr (en) |
| dbp:burnTime |
600.0 (dbd:second) 700.0 (dbd:second) |
| dbp:combustionChamber |
4 (xsd:integer) |
| dbp:countryOfOrigin |
dbr:Soviet_Union |
| dbp:cycle |
dbr:Gas-generator_cycle_(rocket) |
| dbp:date |
1976 (xsd:integer) 1983 (xsd:integer) |
| dbp:designer |
dbr:Yuzhnoye_Design_Bureau |
| dbp:firstDate |
1977-10-31 (xsd:date) March 1986 (en) |
| dbp:fuel |
dbr:UDMH |
| dbp:gimbal |
±55° (en) |
| dbp:manufacturer |
dbr:Yuzhmash |
| dbp:mixtureRatio |
1.800000 (xsd:double) |
| dbp:name |
RD-864 (en) RD-869 (en) |
| dbp:predecessor |
RD-864 (en) |
| dbp:purpose |
Upper stage (en) Upper Stage (en) |
| dbp:restarts |
25 (xsd:integer) 50 (xsd:integer) |
| dbp:status |
In service (en) |
| dbp:successor |
dbr:RD-869 |
| dbp:type |
liquid (en) |
| dbp:usedIn |
R-36M UTTKh and Dnepr third stage (en) R-36M2 third stage (en) |
| dbp:wikiPageUsesTemplate |
dbt:Convert dbt:Infobox_rocket_engine dbt:Nbsp dbt:Reflist dbt:Rocket-stub dbt:Rocket_engines dbt:Short_description dbt:Ubli dbt:N2O4 |
| dct:subject |
dbc:Rocket_engines_of_the_Soviet_Union dbc:Rocket_engines_using_hypergolic_propellant dbc:Rocket_engines_of_Ukraine dbc:Rocket_engines_using_the_gas-generator_cycle dbc:Yuzhmash_rocket_engines dbc:Yuzhnoye_rocket_engines |
| rdfs:comment |
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) |
| rdfs:label |
RD-864 (fr) RD-864 (en) RD-864 (pt) |
| owl:sameAs |
yago-res:RD-864 wikidata:RD-864 dbpedia-fr:RD-864 dbpedia-pt:RD-864 https://global.dbpedia.org/id/2cegL |
| prov:wasDerivedFrom |
wikipedia-en:RD-864?oldid=1100164336&ns=0 |
| foaf:isPrimaryTopicOf |
wikipedia-en:RD-864 |
| is dbo:wikiPageRedirects of |
dbr:15D177 dbr:15D300 dbr:RD-869 |
| is dbo:wikiPageWikiLink of |
dbr:Comparison_of_orbital_rocket_engines dbr:Dnepr_(rocket) dbr:R-36_(missile) dbr:15D177 dbr:15D300 dbr:RD-869 |
| is foaf:primaryTopic of |
wikipedia-en:RD-864 |