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- RD-701 abstract "RD-701 (Russian: Раке́тный дви́гатель 701, Rocket Engine 701) - liquid-fuel rocket engine developed by Energomash, Russia. It was proposed to propel the reusable MAKS space plane before cancellation of this project. The RD-701 is a tripropellant engine that uses staged combustion cycle afterburning of oxidizer-rich hot turbine gas. This engine has two modes: the first one - Mode #1 - uses three components with fuel mixture of RP-1 / LH2 which is applied for near earth surface conditions; the second one - Mode #2 - uses LH2 in vacuum where atmosphere influence is negligible; both of modes uses LOX as an oxidizer.The use of less dense fuel components at maximum efficiency conditions allows minimizing the volume of fuel tanks and subsequently their mass down to 30%. As of 2009 the engine is characterized by highest value of pressure, 300 bar, ever used in combustion chamber of rocket engines when running in Mode #1 with mixture of fuel components. The RD-701 became the base model for RD-704 with one combustion chamber.".
- RD-701 wikiPageExternalLink rd704.htm.
- RD-701 wikiPageExternalLink 40-3.htm.
- RD-701 wikiPageExternalLink rd-701.htm.
- RD-701 wikiPageExternalLink news2_24.html.
- RD-701 wikiPageID "22944222".
- RD-701 wikiPageRevisionID "571297893".
- RD-701 caption "Photo of rocket engine RD-701 exhibited for viewers.".
- RD-701 chamberPressure "Mode#1: 4,351 psi".
- RD-701 chamberPressure "Mode#2: 2,176 psi".
- RD-701 countryOfOrigin Russia.
- RD-701 countryOfOrigin Soviet_Union.
- RD-701 cycle Staged_combustion_cycle.
- RD-701 date "end of 1980 years.".
- RD-701 dryWeight "4240.0".
- RD-701 fuel Liquid_hydrogen.
- RD-701 fuel RP-1.
- RD-701 fuel "Mode#2: LOX / LH2".
- RD-701 hasPhotoCollection RD-701.
- RD-701 imageSize "300".
- RD-701 manufacturer NPO_Energomash.
- RD-701 name "RD-701".
- RD-701 oxidiser "Mode#1: LOX".
- RD-701 specificImpulseSeaLevel "330.0".
- RD-701 specificImpulseVacuum "415.0".
- RD-701 specificImpulseVacuum "460.0".
- RD-701 status "Experimental".
- RD-701 successor "RD-704".
- RD-701 thrust(sl)_ "Mode#1: 714,000 lbf".
- RD-701 thrust(vac)_ "Mode#1: 900,000 lbf".
- RD-701 thrust(vac)_ "Mode#2: 357,000 lbf".
- RD-701 type "liquid".
- RD-701 subject Category:Hydrogen_rocket_engines.
- RD-701 subject Category:Rocket_engines.
- RD-701 comment "RD-701 (Russian: Раке́тный дви́гатель 701, Rocket Engine 701) - liquid-fuel rocket engine developed by Energomash, Russia. It was proposed to propel the reusable MAKS space plane before cancellation of this project. The RD-701 is a tripropellant engine that uses staged combustion cycle afterburning of oxidizer-rich hot turbine gas.".
- RD-701 label "RD-701".
- RD-701 label "RD-701".
- RD-701 label "РД-701".
- RD-701 sameAs RD-701.
- RD-701 sameAs m.063_pb4.
- RD-701 sameAs Q4386509.
- RD-701 sameAs Q4386509.
- RD-701 wasDerivedFrom RD-701?oldid=571297893.
- RD-701 isPrimaryTopicOf RD-701.