RS-56 (original) (raw)
RS-56 era un motor cohete de combustible líquido americano, desarrollado por Rocketdyne. RS-56 se derivó del motor cohete RS-27. Se construyeron dos variantes de este motor, ambos para su uso en la serie de cohetes Atlas II. El primero, RS-56-OBA, era un motor de refuerzo, mientras que el RS-56-OSA se diseñó para usarse como sustentador y producir un empuje más bajo pero a un impulso específico más alto.
| Property | Value |
|---|---|
| dbo:abstract | RS-56 era un motor cohete de combustible líquido americano, desarrollado por Rocketdyne. RS-56 se derivó del motor cohete RS-27. Se construyeron dos variantes de este motor, ambos para su uso en la serie de cohetes Atlas II. El primero, RS-56-OBA, era un motor de refuerzo, mientras que el RS-56-OSA se diseñó para usarse como sustentador y producir un empuje más bajo pero a un impulso específico más alto. (es) RS-56 was an American liquid-fueled rocket engine, developed by Rocketdyne. RS-56 was derived from the RS-27 rocket engine, which itself is derived from the Rocketdyne H-1 rocket engine used in the Saturn I and Saturn IB. Two variants of this engine were built, both for use on the Atlas II rocket series. The first, RS-56-OBA, was a booster engine, while the RS-56-OSA was designed for use as a sustainer and produced lower thrust but at a higher specific impulse. (en) |
| dbo:wikiPageID | 49047024 (xsd:integer) |
| dbo:wikiPageLength | 2662 (xsd:nonNegativeInteger) |
| dbo:wikiPageRevisionID | 1077329777 (xsd:integer) |
| dbo:wikiPageWikiLink | dbr:Rocket dbr:Rocketdyne_H-1 dbr:Saturn_I dbr:Saturn_IB dbr:United_States dbr:Gas-generator_cycle_(rocket) dbc:Rocket_engines_of_the_United_States dbc:Rocket_engines_using_the_gas-generator_cycle dbc:Rocketdyne_engines dbr:Atlas_II dbc:Rocket_engines_using_kerosene_propellant dbr:RP-1 dbr:RS-27 dbr:Specific_impulse dbr:LOX dbr:Rocketdyne |
| dbp:burnTime | 283.0 (dbd:second) RS-56-OBA: 172 (en) |
| dbp:countryOfOrigin | dbr:United_States |
| dbp:cycle | dbr:Gas-generator_cycle_(rocket) |
| dbp:diameter | RS-56-OBA: (en) |
| dbp:firstFlight | 1991 (xsd:integer) |
| dbp:fuel | dbr:RP-1 |
| dbp:length | RS-56-OBA: (en) |
| dbp:manufacturer | dbr:Rocketdyne |
| dbp:name | RS-56 (en) |
| dbp:oxidiser | dbr:LOX |
| dbp:specificImpulseSeaLevel | RS-56-OBA: (en) RS-56-OSA: (en) |
| dbp:specificImpulseVacuum | RS-56-OBA: (en) RS-56-OSA: (en) |
| dbp:status | retired (en) |
| dbp:thrust(sl)_ | RS-56-OBA: (en) RS-56-OSA: (en) |
| dbp:type | liquid (en) |
| dbp:usedIn | dbr:Atlas_II |
| dbp:wikiPageUsesTemplate | dbt:Convert dbt:Infobox_rocket_engine dbt:Reflist dbt:Rocket_engines dbt:Short_description |
| dct:subject | dbc:Rocket_engines_of_the_United_States dbc:Rocket_engines_using_the_gas-generator_cycle dbc:Rocketdyne_engines dbc:Rocket_engines_using_kerosene_propellant |
| gold:hypernym | dbr:Engine |
| rdf:type | dbo:Software |
| rdfs:comment | RS-56 era un motor cohete de combustible líquido americano, desarrollado por Rocketdyne. RS-56 se derivó del motor cohete RS-27. Se construyeron dos variantes de este motor, ambos para su uso en la serie de cohetes Atlas II. El primero, RS-56-OBA, era un motor de refuerzo, mientras que el RS-56-OSA se diseñó para usarse como sustentador y producir un empuje más bajo pero a un impulso específico más alto. (es) RS-56 was an American liquid-fueled rocket engine, developed by Rocketdyne. RS-56 was derived from the RS-27 rocket engine, which itself is derived from the Rocketdyne H-1 rocket engine used in the Saturn I and Saturn IB. Two variants of this engine were built, both for use on the Atlas II rocket series. The first, RS-56-OBA, was a booster engine, while the RS-56-OSA was designed for use as a sustainer and produced lower thrust but at a higher specific impulse. (en) |
| rdfs:label | RS-56 (motor cohete) (es) RS-56 (en) |
| owl:sameAs | yago-res:RS-56 wikidata:RS-56 dbpedia-es:RS-56 https://global.dbpedia.org/id/25cZp |
| prov:wasDerivedFrom | wikipedia-en:RS-56?oldid=1077329777&ns=0 |
| foaf:isPrimaryTopicOf | wikipedia-en:RS-56 |
| is dbo:wikiPageWikiLink of | dbr:MA-5A dbr:Atlas_II dbr:RS-27 dbr:Rocketdyne |
| is dbp:successor of | dbr:RS-27 |
| is foaf:primaryTopic of | wikipedia-en:RS-56 |