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- RD-58 abstract "The RD-58 (manufacturer designation 11D58) is a rocket engine, developed in the 1960s by OKB-1, now RKK Energia. The project was managed by Mikhail Melnikov 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 Buran spacecraft used two descendants of the RD-58 as its main engines.The RD-58 uses LOX as the oxidizer and kerosene as fuel. It features a single gimbaled chamber, radial centrifugal pumps with auxiliary booster pumps, and an oxygen-rich gas generator. Recent modifications include a lightweight carbon-composite nozzle extender.Thrust: 8.5 tf (83.4 kN)Isp: 349 sChamber pressure: 7.8 MPaMass: 300 kgDiameter: 1200 mm".
- RD-58 wikiPageID "7132786".
- RD-58 wikiPageRevisionID "602052222".
- RD-58 auto "yes".
- RD-58 date "December 2009".
- RD-58 hasPhotoCollection RD-58.
- RD-58 subject Category:Kerosene_rocket_engines.
- RD-58 subject Category:Rocket_engines_of_the_Soviet_Union.
- RD-58 comment "The RD-58 (manufacturer designation 11D58) is a rocket engine, developed in the 1960s by OKB-1, now RKK Energia. The project was managed by Mikhail Melnikov 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 (motor de foguete)".
- RD-58 label "RD-58".
- RD-58 label "RD-58".
- 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 sameAs Q1256967.
- RD-58 wasDerivedFrom RD-58?oldid=602052222.
- RD-58 isPrimaryTopicOf RD-58.