Browse Wiki & Semantic Web

Jump to: navigation, search
Http://dbpedia.org/resource/RD-0243
  This page has no properties.
hide properties that link here 
  No properties link to this page.
 
http://dbpedia.org/resource/RD-0243
http://dbpedia.org/ontology/abstract O RD-0243 é um módulo de propulsão compostO RD-0243 é um módulo de propulsão composto de um motor principal RD-0244 e um motor de empuxo vetorial RD-0245. Ambos são alimentados com N2O4 e UDMH. Sendo que o RD-0244 usa um ciclo de combustão em estágios, enquanto o RD-0245 usa o ciclo de geração de gás, mais simples. Como o volume é um luxo em lançamentos submarinos, esse módulo é submerso no tanque de combustível. Ele foi desenvolvido entre 1977 e 1985, tendo sido lançado pela primeira vez em 27 de dezembro de 1981. Originalmente desenvolvido para o , ele foi usado mais tarde no Shtil'.Enquanto o RD-0243, tinha um empuxo de 682 kN, Isp de 280 s, Pressão na câmara de 27,5 MPa e tempo de queima de 74 s, o RD-0245, tinha um empuxo de 211 kN, Isp de 280 s, Pressão na câmara de 14,7 MPa e tempo de queima de 79 s.ara de 14,7 MPa e tempo de queima de 79 s. , Le RD-0243 est un module de propulsion comLe RD-0243 est un module de propulsion composé d'un moteur principal RD-0244 et d'un moteur vernier RD-0245. Tous deux sont des moteurs-fusées à ergols liquides, brûlant de l'UDMH et du N2O4. Le moteur principal RD-0244 fonctionne selon le cycle à combustion étagée riche en oxydant, tandis que le moteur vernier RD-0245 utilise le cycle générateur de gaz, plus simple. Puisque l'encombrement est une priorité pour les missiles embarqués dans les sous-marins, ce module est immergé dans le réservoir de carburant. Sa période de développement alla de 1977 à 1985, son premier vol ayant eu lieu le 27 décembre 1981. Initialement développé pour le missile RSM-54, il fut ensuite utilisé sur le lanceur Shtil', issu de la reconversion du missile.htil', issu de la reconversion du missile. , The RD-0243 is a propulsion module composeThe RD-0243 is a propulsion module composed of an RD-0244 main engine and a RD-0245 vernier engine. Both are liquid rocket engine, burning N2O4 and UDMH. The RD-0244 main engine operates in the oxidizer rich staged combustion cycle, while the vernier RD-0245 uses the simpler gas generator cycle. Since volume is at a premium on submarine launches, this module is submerged on the propellant tank. Its development period was from 1977 to 1985, having had its first launch on December 27, 1981. Originally developed for the RSM-54, it was used later for the Shtil'. RSM-54, it was used later for the Shtil'. , RD-0243はRD-0244主エンジンとRD-0245バーニアスラスタを組み合わせた推進モジュールである。両方ともN2O4とUDMHを燃焼する液体ロケットエンジンである。RD-0244主エンジンは酸化剤リッチ二段燃焼サイクルでバーニアの RD-0245は単純なガス発生器サイクルを採用する。体積の制限のある潜水艦から発射されるためモジュールは推進剤タンク内に沈められる。 開発されたのは1977年から1985年で最初の打ち上げは1981年12月27日だった。原型機はのために開発され、後にで使用された。
http://dbpedia.org/ontology/wikiPageExternalLink https://web.archive.org/web/20140504224815/http:/www.kbkha.ru/%3Fp=8&cat=10&prod=50 + , https://web.archive.org/web/20150824113800/http:/www.astronautix.com/engines/rd0243.htm +
http://dbpedia.org/ontology/wikiPageID 47016009
http://dbpedia.org/ontology/wikiPageLength 6164
http://dbpedia.org/ontology/wikiPageRevisionID 1100134924
http://dbpedia.org/ontology/wikiPageWikiLink http://dbpedia.org/resource/Vernier_thruster + , http://dbpedia.org/resource/Staged_combustion_cycle_%28rocket%29 + , http://dbpedia.org/resource/Gas-generator_cycle_%28rocket%29 + , http://dbpedia.org/resource/Category:Sea_launch_to_orbit + , http://dbpedia.org/resource/Category:Rocket_engines_using_hypergolic_propellant + , http://dbpedia.org/resource/Liquid-fuel_rocket + , http://dbpedia.org/resource/Unsymmetrical_dimethylhydrazine + , http://dbpedia.org/resource/R-29RM_Shtil + , http://dbpedia.org/resource/Shtil%27 + , http://dbpedia.org/resource/USSR + , http://dbpedia.org/resource/KBKhA + , http://dbpedia.org/resource/Category:KBKhA_rocket_engines + , http://dbpedia.org/resource/Category:Rocket_engines_of_the_Soviet_Union + , http://dbpedia.org/resource/Rocket_engine + , http://dbpedia.org/resource/Dinitrogen_tetroxide + , http://dbpedia.org/resource/Category:Rocket_engines_using_the_staged_combustion_cycle +
http://dbpedia.org/property/associated http://dbpedia.org/resource/R-29RM_Shtil + , http://dbpedia.org/resource/Shtil%27 +
http://dbpedia.org/property/burnTime 74.0 , 79.0
http://dbpedia.org/property/combustionChamber 1 , 4
http://dbpedia.org/property/countryOfOrigin http://dbpedia.org/resource/USSR +
http://dbpedia.org/property/cycle http://dbpedia.org/resource/Staged_combustion_cycle_%28rocket%29 + , http://dbpedia.org/resource/Gas-generator_cycle_%28rocket%29 +
http://dbpedia.org/property/designer http://dbpedia.org/resource/KBKhA +
http://dbpedia.org/property/firstDate "1981-12-27"^^xsd:date
http://dbpedia.org/property/fuel http://dbpedia.org/resource/Unsymmetrical_dimethylhydrazine +
http://dbpedia.org/property/mixtureRatio 2.6
http://dbpedia.org/property/name RD-0244 , RD-0245
http://dbpedia.org/property/nozzleRatio 14
http://dbpedia.org/property/oxidiser http://dbpedia.org/resource/Dinitrogen_tetroxide +
http://dbpedia.org/property/status Retired
http://dbpedia.org/property/type liquid
http://dbpedia.org/property/usedIn RD-0243 Propulsion Module
http://dbpedia.org/property/wikiPageUsesTemplate http://dbpedia.org/resource/Template:Reflist + , http://dbpedia.org/resource/Template:Portal + , http://dbpedia.org/resource/Template:Infobox_rocket_engine + , http://dbpedia.org/resource/Template:Rocket_engines + , http://dbpedia.org/resource/Template:Convert + , http://dbpedia.org/resource/Template:Rocket-stub +
http://purl.org/dc/terms/subject http://dbpedia.org/resource/Category:Rocket_engines_using_the_staged_combustion_cycle + , http://dbpedia.org/resource/Category:Sea_launch_to_orbit + , http://dbpedia.org/resource/Category:Rocket_engines_of_the_Soviet_Union + , http://dbpedia.org/resource/Category:Rocket_engines_using_hypergolic_propellant + , http://dbpedia.org/resource/Category:KBKhA_rocket_engines +
http://purl.org/linguistics/gold/hypernym http://dbpedia.org/resource/Module +
http://www.w3.org/ns/prov#wasDerivedFrom http://en.wikipedia.org/wiki/RD-0243?oldid=1100134924&ns=0 +
http://xmlns.com/foaf/0.1/homepage https://web.archive.org/web/20140504224815/http:/www.kbkha.ru/%3Fp=8&cat=10&prod=50 +
http://xmlns.com/foaf/0.1/isPrimaryTopicOf http://en.wikipedia.org/wiki/RD-0243 +
owl:sameAs http://yago-knowledge.org/resource/RD-0243 + , http://pt.dbpedia.org/resource/RD-0243 + , http://ja.dbpedia.org/resource/RD-0243 + , http://dbpedia.org/resource/RD-0243 + , http://www.wikidata.org/entity/Q20203125 + , http://rdf.freebase.com/ns/m.013f7c6c + , http://fr.dbpedia.org/resource/RD-0243 + , https://global.dbpedia.org/id/utAV +
rdf:type http://dbpedia.org/ontology/Software +
rdfs:comment The RD-0243 is a propulsion module composeThe RD-0243 is a propulsion module composed of an RD-0244 main engine and a RD-0245 vernier engine. Both are liquid rocket engine, burning N2O4 and UDMH. The RD-0244 main engine operates in the oxidizer rich staged combustion cycle, while the vernier RD-0245 uses the simpler gas generator cycle. Since volume is at a premium on submarine launches, this module is submerged on the propellant tank. Its development period was from 1977 to 1985, having had its first launch on December 27, 1981. Originally developed for the RSM-54, it was used later for the Shtil'. RSM-54, it was used later for the Shtil'. , Le RD-0243 est un module de propulsion comLe RD-0243 est un module de propulsion composé d'un moteur principal RD-0244 et d'un moteur vernier RD-0245. Tous deux sont des moteurs-fusées à ergols liquides, brûlant de l'UDMH et du N2O4. Le moteur principal RD-0244 fonctionne selon le cycle à combustion étagée riche en oxydant, tandis que le moteur vernier RD-0245 utilise le cycle générateur de gaz, plus simple. Puisque l'encombrement est une priorité pour les missiles embarqués dans les sous-marins, ce module est immergé dans le réservoir de carburant. Sa période de développement alla de 1977 à 1985, son premier vol ayant eu lieu le 27 décembre 1981. Initialement développé pour le missile RSM-54, il fut ensuite utilisé sur le lanceur Shtil', issu de la reconversion du missile.htil', issu de la reconversion du missile. , RD-0243はRD-0244主エンジンとRD-0245バーニアスラスタを組み合わせた推進モジュールである。両方ともN2O4とUDMHを燃焼する液体ロケットエンジンである。RD-0244主エンジンは酸化剤リッチ二段燃焼サイクルでバーニアの RD-0245は単純なガス発生器サイクルを採用する。体積の制限のある潜水艦から発射されるためモジュールは推進剤タンク内に沈められる。 開発されたのは1977年から1985年で最初の打ち上げは1981年12月27日だった。原型機はのために開発され、後にで使用された。 , O RD-0243 é um módulo de propulsão compostO RD-0243 é um módulo de propulsão composto de um motor principal RD-0244 e um motor de empuxo vetorial RD-0245. Ambos são alimentados com N2O4 e UDMH. Sendo que o RD-0244 usa um ciclo de combustão em estágios, enquanto o RD-0245 usa o ciclo de geração de gás, mais simples. Como o volume é um luxo em lançamentos submarinos, esse módulo é submerso no tanque de combustível. Ele foi desenvolvido entre 1977 e 1985, tendo sido lançado pela primeira vez em 27 de dezembro de 1981. Originalmente desenvolvido para o , ele foi usado mais tarde no Shtil'.Enquanto o RD-0243, tinha um empuxo de 682 kN, Isp de 280 s, Pressão na câmara de 27,5 MPa e tempo de queima de 74 s, o RD-0245, tinha um empuxo de 211 kN, Isp de 280 s, Pressão na câmara de 14,7 MPa e tempo de queima de 79 s.ara de 14,7 MPa e tempo de queima de 79 s.
rdfs:label RD-0243
hide properties that link here 
http://dbpedia.org/resource/RD-0244 + http://dbpedia.org/ontology/wikiPageRedirects
http://dbpedia.org/resource/Chemical_Automatics_Design_Bureau + , http://dbpedia.org/resource/RD-0244 + , http://dbpedia.org/resource/RD-0245 + http://dbpedia.org/ontology/wikiPageWikiLink
http://en.wikipedia.org/wiki/RD-0243 + http://xmlns.com/foaf/0.1/primaryTopic
http://dbpedia.org/resource/RD-0243 + owl:sameAs
 

 

Enter the name of the page to start semantic browsing from.