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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. Mode #1 uses three components: LOX as an oxidizer and a fuel mixture of RP-1 / LH2 which is applied for near earth surface conditions. Mode #2 also uses LOX, with LH2 as fuel in vacuum where atmospheric influence is negligible.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 wikiPageLength "4881".
- RD-701 wikiPageOutDegree "59".
- RD-701 wikiPageRevisionID "706930609".
- RD-701 wikiPageWikiLink Bar_(unit).
- RD-701 wikiPageWikiLink Category:Rocket_engines_of_Russia.
- RD-701 wikiPageWikiLink Category:Rocket_engines_of_the_Soviet_Union.
- RD-701 wikiPageWikiLink Category:Rocket_engines_using_hydrogen_propellant.
- RD-701 wikiPageWikiLink Combustion_chamber.
- RD-701 wikiPageWikiLink Fuel.
- RD-701 wikiPageWikiLink Kilogram.
- RD-701 wikiPageWikiLink Liquid-propellant_rocket.
- RD-701 wikiPageWikiLink Liquid_hydrogen.
- RD-701 wikiPageWikiLink Liquid_oxygen.
- RD-701 wikiPageWikiLink MAKS_(spacecraft).
- RD-701 wikiPageWikiLink NPO_Energomash.
- RD-701 wikiPageWikiLink Newton_(unit).
- RD-701 wikiPageWikiLink Oxidizing_agent.
- RD-701 wikiPageWikiLink Pascal_(unit).
- RD-701 wikiPageWikiLink Pound_(force).
- RD-701 wikiPageWikiLink Pound_(mass).
- RD-701 wikiPageWikiLink Pounds_per_square_inch.
- RD-701 wikiPageWikiLink RD-0120.
- RD-701 wikiPageWikiLink RD-170.
- RD-701 wikiPageWikiLink RP-1.
- RD-701 wikiPageWikiLink Regenerative_cooling.
- RD-701 wikiPageWikiLink Rocket_engine.
- RD-701 wikiPageWikiLink Russia.
- RD-701 wikiPageWikiLink Second.
- RD-701 wikiPageWikiLink Soviet_Union.
- RD-701 wikiPageWikiLink Specific_impulse.
- RD-701 wikiPageWikiLink Staged_combustion_cycle.
- RD-701 wikiPageWikiLink Turbine.
- RD-701 wikiPageWikiLinkText "RD-701".
- 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 "late 1980's".
- RD-701 dryWeight "4240.0".
- RD-701 fuel Liquid_hydrogen.
- RD-701 fuel RP-1.
- RD-701 fuel "Mode#2: LOX / LH2".
- 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 wikiPageUsesTemplate Template:Clarify.
- RD-701 wikiPageUsesTemplate Template:Convert.
- RD-701 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- RD-701 wikiPageUsesTemplate Template:Lang-ru.
- RD-701 subject Category:Rocket_engines_of_Russia.
- RD-701 subject Category:Rocket_engines_of_the_Soviet_Union.
- RD-701 subject Category:Rocket_engines_using_hydrogen_propellant.
- RD-701 type Technology.
- 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. This engine has two modes. Mode #1 uses three components: LOX as an oxidizer and a fuel mixture of RP-1 / LH2 which is applied for near earth surface conditions.".
- RD-701 label "RD-701".
- RD-701 sameAs Q4386509.
- RD-701 sameAs RD-701.
- RD-701 sameAs m.063_pb4.
- RD-701 sameAs РД-701.
- RD-701 sameAs Q4386509.
- RD-701 wasDerivedFrom RD-701?oldid=706930609.
- RD-701 isPrimaryTopicOf RD-701.