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- RD-58 abstract "The RD-58 (manufacturer designation 11D58) was a rocket engine, developed in the 1960s by OKB-1, now RKK Energia. The project was managed by Mikhail Melnikov, and it was based on the previous S1.5400 which was the first stage combustion engine in the world. The engine was initially created to power the Block D stage of the Soviet Union's abortive N-1 rocket. Derivatives of this stage are now used as upper stages on some Proton and Zenit rockets. An alternative version of the RD-58 chamber, featuring a shorter nozzle, was used as the N-1's roll-control engine.The RD-58 uses LOX as the oxidizer and RG-1 as fuel in an oxidizer rich stage combustion cycle. It features a single gimbaled chamber, radial centrifugal pumps with auxiliary booster pumps, and an oxygen-rich preburner. Recent modifications include a lightweight carbon-composite nozzle extender developed by NPO Iskra.The Buran spacecraft used two of an evolution of the RD-58M, called 17D12, as its main orbital correction engines. Instead of RG-1, it burned Syntin, and could be ignited 15 times. It is assumed that it was the base for the RD-58S, which had practically the same specifications and powered the Blok DM-2M. But the manufacturer states that the engine is compatible with both propellants.The current version of the engine is the RD-58M (manufacturer designation 11D58M), which has slightly reduced thrust, but increased isp. An even newer version is under development and is known as the RD-58MF (manufacturer designation 11D58MF). It will reduce thrust to 49.03 kilonewtons (11,020 lbf) to keep the same length but increase expansion ratio to 500:1. This will enable it to gain 20s of isp (to an expected 372s). It will eventually fly on the Blok DM-03. This new version of the engine will be built in the Krasnoyarsk Machine-Building Plant. During a November 2014 interview, Vladimir Kolmykov, the Deputy General Director of the Chemical Division of Krasnoyarsk Machine-Building Plant, stated that the production of Block-DM was suspended during that year, but work on the stage and development of the RD-58MF will resume during 2015.".
- RD-58 wikiPageID "7132786".
- RD-58 wikiPageLength "16608".
- RD-58 wikiPageOutDegree "94".
- RD-58 wikiPageRevisionID "697590150".
- RD-58 wikiPageWikiLink 17D11.
- RD-58 wikiPageWikiLink Blok_D.
- RD-58 wikiPageWikiLink Blok_DM-03.
- RD-58 wikiPageWikiLink Buran_(spacecraft).
- RD-58 wikiPageWikiLink Buran_programme.
- RD-58 wikiPageWikiLink Category:Rocket_engines.
- RD-58 wikiPageWikiLink Category:Rocket_engines_of_Russia.
- RD-58 wikiPageWikiLink Category:Rocket_engines_of_the_Soviet_Union.
- RD-58 wikiPageWikiLink Category:Rocket_engines_using_kerosene_propellant.
- RD-58 wikiPageWikiLink Category:Spaceflight.
- RD-58 wikiPageWikiLink Centrifugal_pump.
- RD-58 wikiPageWikiLink Fuel.
- RD-58 wikiPageWikiLink GRAU.
- RD-58 wikiPageWikiLink Gimbal.
- RD-58 wikiPageWikiLink JSC_Krasnoyarsk_Machine-Building_Plant.
- RD-58 wikiPageWikiLink Liquid-propellant_rocket.
- RD-58 wikiPageWikiLink Liquid_oxygen.
- RD-58 wikiPageWikiLink Mikhail_Melnikov.
- RD-58 wikiPageWikiLink Multistage_rocket.
- RD-58 wikiPageWikiLink N1_(rocket).
- RD-58 wikiPageWikiLink Nozzle_extension.
- RD-58 wikiPageWikiLink Oxidizing_agent.
- RD-58 wikiPageWikiLink Proton-K.
- RD-58 wikiPageWikiLink Proton-M.
- RD-58 wikiPageWikiLink Proton_(rocket_family).
- RD-58 wikiPageWikiLink RP-1.
- RD-58 wikiPageWikiLink Reinforced_carbon–carbon.
- RD-58 wikiPageWikiLink Rocket_engine.
- RD-58 wikiPageWikiLink S.P._Korolev_Rocket_and_Space_Corporation_Energia.
- RD-58 wikiPageWikiLink S1.5400.
- RD-58 wikiPageWikiLink Soviet_Union.
- RD-58 wikiPageWikiLink Staged_combustion_cycle.
- RD-58 wikiPageWikiLink Syntin.
- RD-58 wikiPageWikiLink Thuraya.
- RD-58 wikiPageWikiLink Voronezh_Mechanical_Plant.
- RD-58 wikiPageWikiLink Zenit-3SL.
- RD-58 wikiPageWikiLink Zenit_(rocket_family).
- RD-58 wikiPageWikiLinkText "RD-58".
- RD-58 associated N1_(rocket).
- RD-58 associated Proton-K.
- RD-58 associated Proton-M.
- RD-58 associated Zenit_(rocket_family).
- RD-58 burnTime "600.0".
- RD-58 combustionChamber "1".
- RD-58 countryOfOrigin Soviet_Union.
- RD-58 cycle Staged_combustion_cycle.
- RD-58 designer Mikhail_Melnikov.
- RD-58 designer S.P._Korolev_Rocket_and_Space_Corporation_Energia.
- RD-58 firstDate "1967".
- RD-58 fuel RP-1.
- RD-58 manufacturer Voronezh_Mechanical_Plant.
- RD-58 name "RD-58M".
- RD-58 oxidiser Liquid_oxygen.
- RD-58 predecessor S1.5400.
- RD-58 purpose "Upper Stage".
- RD-58 specificImpulseVacuum "353.0".
- RD-58 status "In Production".
- RD-58 type "liquid".
- RD-58 usedIn Blok_D.
- RD-58 wikiPageUsesTemplate Template:Convert.
- RD-58 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- RD-58 wikiPageUsesTemplate Template:Orbital_spacecraft_rocket_engines.
- RD-58 wikiPageUsesTemplate Template:Reflist.
- RD-58 wikiPageUsesTemplate Template:Rocket_Engines.
- RD-58 wikiPageUsesTemplate Template:Russian_and_Soviet_military_designation_sequences.
- RD-58 subject Category:Rocket_engines.
- RD-58 subject Category:Rocket_engines_of_Russia.
- RD-58 subject Category:Rocket_engines_of_the_Soviet_Union.
- RD-58 subject Category:Rocket_engines_using_kerosene_propellant.
- RD-58 subject Category:Spaceflight.
- RD-58 hypernym Engine.
- RD-58 type Software.
- RD-58 type Redirect.
- RD-58 comment "The RD-58 (manufacturer designation 11D58) was a rocket engine, developed in the 1960s by OKB-1, now RKK Energia. The project was managed by Mikhail Melnikov, and it was based on the previous S1.5400 which was the first stage combustion engine in the world. The engine was initially created to power the Block D stage of the Soviet Union's abortive N-1 rocket. Derivatives of this stage are now used as upper stages on some Proton and Zenit rockets.".
- RD-58 label "RD-58".
- RD-58 sameAs Q1256967.
- RD-58 sameAs 17D12.
- RD-58 sameAs RD-58.
- RD-58 sameAs RD-58.
- RD-58 sameAs RD-58_(motor_de_foguete).
- RD-58 sameAs m.0h5wp6.
- RD-58 sameAs Q1256967.
- RD-58 wasDerivedFrom RD-58?oldid=697590150.
- RD-58 isPrimaryTopicOf RD-58.