Matches in DBpedia 2014 for { ?s ?p 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.. }
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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.".