KTDU-35 (original) (raw)
O KTDU-35 (também conhecido como 11D62), foi um sistema de propulsão soviético, composto por dois motores de foguete a combustível líquido. O primário S5.60 (SKD) e o secundário S5.35 (DKD), abastecidos pelos mesmos tanques queimando UDMH e AK27I num ciclo de geração de gás. Ele foi projetado por e desenvolvido no para o Programa Soyuz.
| Property | Value |
|---|---|
| dbo:abstract | The KTDU-35 (GRAU Index 11D62) was a Soviet spacecraft propulsion system composed of two liquid rocket engines, the primary, S5.60 (SKD) and the secondary S5.35 (DKD), fed from the same propellant tanks. Both engines burn UDMH and AK27I in the gas generator cycle. It was designed by OKB-2, the famous Isaev Design Bureau, for the original Soyuz programme. Within the Soyuz and Progress, the SKD is the primary engine, the DKD is the backup engine for main orbital correction and de-orbit operations. The engine generate 4.09 kN (920 lbf) (SKD) or 4.03 kN (910 lbf) (DKD) of thrust with a specific impulse of 278 seconds and 270 seconds, respectively. The SKD nozzle is fixed in the aft of the craft, and the dual DKD nozzles are on either side. The spacecraft attitude system (DPO) is responsible for pointing the vehicle in the correct direction and keep it that way during SKD burns. (en) O KTDU-35 (também conhecido como 11D62), foi um sistema de propulsão soviético, composto por dois motores de foguete a combustível líquido. O primário S5.60 (SKD) e o secundário S5.35 (DKD), abastecidos pelos mesmos tanques queimando UDMH e AK27I num ciclo de geração de gás. Ele foi projetado por e desenvolvido no para o Programa Soyuz. (pt) |
| dbo:wikiPageExternalLink | http://kbhmisaeva.ru/main.php%3Fid=53 |
| dbo:wikiPageID | 47348378 (xsd:integer) |
| dbo:wikiPageLength | 6621 (xsd:nonNegativeInteger) |
| dbo:wikiPageRevisionID | 1084020183 (xsd:integer) |
| dbo:wikiPageWikiLink | dbr:Progress_(spacecraft) dbr:Salyut_1 dbr:Salyut_4 dbr:Aleksei_Mihailovich_Isaev dbr:Unsymmetrical_dimethylhydrazine dbr:Soyuz_programme dbr:KB_KhIMMASH dbc:Rocket_engines_of_Russia dbc:Rocket_engines_of_the_Soviet_Union dbc:Rocket_engines_using_hypergolic_propellant dbr:S5.4 dbr:Gas-generator_cycle dbr:GRAU dbr:USSR dbr:KTDU-426 dbr:Soviet_Union dbr:Soyuz_7K-LOK dbr:Soyuz_7K-OK dbr:Soyuz_7K-OKS dbr:Soyuz_7K-TM dbr:Kosmos_133 dbr:Red_fuming_nitric_acid dbr:Specific_impulse dbr:Low_Earth_orbit dbr:Soyuz_(spacecraft) dbr:Progress_7K-TG dbr:Rocket_engine dbr:Soyuz_7K-T dbr:Soviet_crewed_lunar_programs dbr:Liquid-fuel_rocket |
| dbp:burnTime | 500.0 (dbd:second) |
| dbp:chamberPressure | S5.60: (en) |
| dbp:combustionChamber | S5.35: 2 (en) S5.60: 1 (en) |
| dbp:countryOfOrigin | dbr:USSR |
| dbp:cycle | dbr:Gas-generator_cycle |
| dbp:date | 1962 (xsd:integer) |
| dbp:designer | OKB-2, Anton Tavzarachvili (en) |
| dbp:firstDate | 1966-11-28 (xsd:date) |
| dbp:fuel | dbr:Unsymmetrical_dimethylhydrazine |
| dbp:mixtureRatio | 1.850000 (xsd:double) |
| dbp:name | KTDU-35 (en) |
| dbp:oxidiser | dbr:Red_fuming_nitric_acid |
| dbp:predecessor | dbr:S5.4 |
| dbp:purpose | Spacecraft main propulsion (en) |
| dbp:restarts | 25 (xsd:integer) |
| dbp:specificImpulseVacuum | 270.0 (dbd:second) 278.0 (dbd:second) |
| dbp:status | Retired (en) |
| dbp:successor | dbr:KTDU-426 |
| dbp:thrust(vac)_ | S5.35: (en) S5.60: (en) |
| dbp:type | liquid (en) |
| dbp:usedIn | Soyuz from 7K-OK to 7K-T and Progress 7K-TG (en) |
| dbp:wikiPageUsesTemplate | dbt:Convert dbt:Infobox_rocket_engine dbt:Orbital_spacecraft_rocket_engines dbt:Reflist dbt:Rocket-stub |
| dct:subject | dbc:Rocket_engines_of_Russia dbc:Rocket_engines_of_the_Soviet_Union dbc:Rocket_engines_using_hypergolic_propellant |
| gold:hypernym | dbr:System |
| rdfs:comment | O KTDU-35 (também conhecido como 11D62), foi um sistema de propulsão soviético, composto por dois motores de foguete a combustível líquido. O primário S5.60 (SKD) e o secundário S5.35 (DKD), abastecidos pelos mesmos tanques queimando UDMH e AK27I num ciclo de geração de gás. Ele foi projetado por e desenvolvido no para o Programa Soyuz. (pt) The KTDU-35 (GRAU Index 11D62) was a Soviet spacecraft propulsion system composed of two liquid rocket engines, the primary, S5.60 (SKD) and the secondary S5.35 (DKD), fed from the same propellant tanks. Both engines burn UDMH and AK27I in the gas generator cycle. It was designed by OKB-2, the famous Isaev Design Bureau, for the original Soyuz programme. (en) |
| rdfs:label | KTDU-35 (en) KTDU-35 (pt) |
| owl:sameAs | yago-res:KTDU-35 wikidata:KTDU-35 dbpedia-gl:KTDU-35 dbpedia-pt:KTDU-35 https://global.dbpedia.org/id/yZn7 |
| prov:wasDerivedFrom | wikipedia-en:KTDU-35?oldid=1084020183&ns=0 |
| foaf:homepage | http://kbhmisaeva.ru/main.php%3Fid=53 |
| foaf:isPrimaryTopicOf | wikipedia-en:KTDU-35 |
| is dbo:wikiPageRedirects of | dbr:S5.35 dbr:S5.53 dbr:S5.60 dbr:S5.66 dbr:KTDU-66 dbr:11D62 |
| is dbo:wikiPageWikiLink of | dbr:11D428 dbr:S5.80 dbr:A.M._Isayev_Chemical_Engineering_Design_Bureau dbr:KTDU-80 dbr:S5.35 dbr:S5.53 dbr:S5.60 dbr:S5.66 dbr:KTDU-66 dbr:11D62 |
| is dbp:predecessor of | dbr:KTDU-80 |
| is foaf:primaryTopic of | wikipedia-en:KTDU-35 |