| dbo:description |
Raketentriebwerk für Flüssigkeitsraketen (de) liquid-fuel rocket engine (en) |
| dbo:thumbnail |
wiki-commons:Special:FilePath/Mockup_rocket_motor_R...u_Bourget_2013_DSC_0062.jpg?width=300 |
| dbo:wikiPageWikiLink |
dbr:Thrust dbr:Specific_impulse dbr:Second dbc:Energomash_rocket_engines dbc:Rocket_engines_of_the_Soviet_Union dbr:Universal_Rocket dbr:Perm,_Russia dbr:Russia dbr:Soviet_Union dbr:Geostationary_orbit dbr:Luna_programme dbr:Venera dbr:Proton-K dbr:Proton-M dbr:N1_(rocket) dbr:NPO_Energomash dbc:Rocket_engines_of_Russia dbc:Rocket_engines_using_the_staged_combustion_cycle dbc:Rocket_engines_using_hypergolic_propellant dbr:Valentin_Glushko dbr:Rocket_engine dbr:Unsymmetrical_dimethylhydrazine dbr:Combustion_chamber dbr:R-36_(missile) dbr:Dinitrogen_tetroxide dbr:Liquid-propellant_rocket dbr:Mir dbr:Space_mission dbr:USD dbr:Proton_(rocket) dbr:Proton-PM dbr:USSR dbr:GRAU dbr:Orbital_station dbr:Staged_combustion_cycle_(rocket) dbr:ISS dbr:Mars_probe_program dbr:Hypergolic dbr:Payload_(air_and_space_craft) dbr:Salyut_program |
| dbp:associated |
dbr:Proton_(rocket_family) |
| dbp:caption |
Mock-up of a RD-275 rocket motor at the Paris Air Show in 2013 (en) |
| dbp:chamberPressure |
RD-253: (en) RD-275: (en) RD-275M: (en) |
| dbp:combustionChamber |
1 (xsd:integer) |
| dbp:cycle |
dbr:Staged_combustion_cycle |
| dbp:designer |
dbr:NPO_Energomash dbr:Valentin_Glushko |
| dbp:dryWeight |
RD-253: (en) RD-275: (en) RD-275M: (en) |
| dbp:firstDate |
RD-253: 1965 (en) RD-275: 1995 (en) RD-275М: 2007 (en) |
| dbp:fuel |
dbr:Unsymmetrical_dimethylhydrazine |
| dbp:gimbal |
7.500000 (xsd:double) |
| dbp:manufacturer |
dbr:Proton-PM |
| dbp:mixtureRatio |
2.670000 (xsd:double) |
| dbp:name |
RD-253 (en) |
| dbp:nozzleRatio |
26.200000 (xsd:double) |
| dbp:purpose |
First stage booster (en) |
| dbp:specificImpulseSeaLevel |
285.0 (dbd:second) 287.0 (dbd:second) 288.0 (dbd:second) |
| dbp:specificImpulseVacuum |
316.0 (dbd:second) 315.8 (dbd:second) |
| dbp:status |
Operational (en) |
| dbp:successor |
RD-254, RD-256, RD-275, RD-275М (en) |
| dbp:thrust(sl) |
RD-253: (en) RD-275: (en) RD-275М: (en) |
| dbp:thrust(vac) |
RD-253: (en) RD-275: (en) RD-275М: (en) |
| dbp:thrustToWeight |
156.200000 (xsd:double) |
| dbp:type |
liquid (en) |
| dbp:wikiPageUsesTemplate |
dbt:Reflist dbt:Small dbt:RUS dbt:Infobox_rocket_engine dbt:Rocket_engines dbt:Convert dbt:Chem2 dbt:Citation_needed dbt:Which dbt:Cvt dbt:USSR dbt:Langx dbt:Short_description dbt:N2O4 |
| dct:subject |
dbc:Energomash_rocket_engines dbc:Rocket_engines_of_the_Soviet_Union dbc:Rocket_engines_of_Russia dbc:Rocket_engines_using_the_staged_combustion_cycle dbc:Rocket_engines_using_hypergolic_propellant |
| gold:hypernym |
dbr:Engines |
| rdfs:label |
RD-253 (en) RD-253 (ca) RD-253 (de) RD-253 (in) RD-253 (fr) RD-253 (ja) RD-253 (pl) RD-253 (pt) РД-253 (ru) RD-253火箭发动机 (zh) |
| owl:sameAs |
freebase:RD-253 yago-res:RD-253 wikidata:RD-253 dbpedia-de:RD-253 dbpedia-fr:RD-253 dbpedia-zh:RD-253 dbpedia-ja:RD-253 dbpedia-pt:RD-253 dbpedia-ru:RD-253 dbpedia-pl:RD-253 dbpedia-id:RD-253 dbpedia-ca:RD-253 dbpedia-gl:RD-253 dbpedia-global:RD-253 |
| prov:wasDerivedFrom |
wikipedia-en:RD-253?oldid=1263842401&ns=0 |
| foaf:depiction |
wiki-commons:Special:FilePath/Mockup_rocket_motor_RD-275_Salon_du_Bourget_2013_DSC_0062.jpg |
| foaf:isPrimaryTopicOf |
wikipedia-en:RD-253 |
| is dbo:wikiPageRedirects of |
dbr:11D43 dbr:14D14 dbr:14D14M dbr:RD-220 dbr:RD-221 dbr:RD-222 dbr:RD-223 dbr:RD-254 dbr:RD-256 dbr:RD-275 dbr:RD-275M dbr:RD-276 |
| is dbo:wikiPageWikiLink of |
dbr:Staged_combustion_cycle dbr:RD-270 dbr:Vladimir_Chelomey dbr:Proton-K dbr:Proton-M dbr:NPO_Energomash dbr:NK-33 dbr:Proton-PM dbr:R-56_(rocket) dbr:11D43 dbr:14D14 dbr:14D14M dbr:RD-220 dbr:RD-221 dbr:RD-222 dbr:RD-223 dbr:RD-254 dbr:RD-256 dbr:RD-275 dbr:RD-275M dbr:RD-276 |
| is foaf:primaryTopic of |
wikipedia-en:RD-253 |
