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  2. RP-1 - Wikipedia

    en.wikipedia.org/wiki/RP-1

    RP-1 (Rocket Propellant-1 or Refined Petroleum-1) and similar fuels like RG-1 and T-1 are highly refined kerosene formulations used as rocket fuel. Liquid-fueled rockets that use RP-1 as fuel are known as kerolox rockets. In their engines, RP-1 is atomized, mixed with liquid oxygen (LOX), and ignited to produce thrust.

  3. Liquid-propellant rocket - Wikipedia

    en.wikipedia.org/wiki/Liquid-propellant_rocket

    Liquid rocket engines have tankage and pipes to store and transfer propellant, an injector system and one or more combustion chambers with associated nozzles.. Typical liquid propellants have densities roughly similar to water, approximately 0.7 to 1.4 g/cm 3 (0.025 to 0.051 lb/cu in).

  4. Rutherford (rocket engine) - Wikipedia

    en.wikipedia.org/wiki/Rutherford_(rocket_engine)

    Rutherford is a liquid-propellant rocket engine designed by aerospace company Rocket Lab [8] and manufactured in Long Beach, California. [9] The engine is used on the company's own rocket, Electron. It uses LOX (liquid oxygen) and RP-1 (refined kerosene) as its propellants and is the first flight-ready engine to use the electric-pump-fed cycle.

  5. Rocket propellant - Wikipedia

    en.wikipedia.org/wiki/Rocket_propellant

    The rocket is launched using liquid hydrogen and liquid oxygen cryogenic propellants. Rocket propellant is used as reaction mass ejected from a rocket engine to produce thrust. The energy required can either come from the propellants themselves, as with a chemical rocket, or from an external source, as with ion engines.

  6. Liquid rocket propellant - Wikipedia

    en.wikipedia.org/wiki/Liquid_rocket_propellant

    The rocket, developed by Relativity Space, uses the Aeon 1 engine. Starship achieved a transatmospheric orbit on its third flight on 14 March 2024, [27] after two failed attempts. The rocket, developed by SpaceX, uses the Raptor engine. SpaceX developed the Raptor engine for its Starship super-heavy-lift launch vehicle. [28]

  7. Rocketdyne H-1 - Wikipedia

    en.wikipedia.org/wiki/Rocketdyne_H-1

    The Rocketdyne H-1 was a 205,000 lbf (910 kN) thrust liquid-propellant rocket engine burning LOX and RP-1.The H-1 was developed for use in the S-I and S-IB first stages of the Saturn I and Saturn IB rockets, respectively, where it was used in clusters of eight engines.

  8. RD-180 - Wikipedia

    en.wikipedia.org/wiki/RD-180

    'Rocket Engine-180') is a rocket engine that was designed and built in Russia. It features a dual combustion chamber , dual- nozzle design and is fueled by a RP-1 / LOX mixture. The RD-180 is derived from the RD-170 line of rocket engines, which were used in the Soviet Energia launch vehicle .

  9. RP 1 - Wikipedia

    en.wikipedia.org/wiki/RP_1

    RP 1, RP-1, RP.1, RP1, or similar terms may refer to: DZRB-AM, a Philippine radio station known as Radyo Pilipinas 1 or RP1 News; RP-1, Rocket Propellant 1; RP1, retinitis pigmentosa 1 protein; RP1 asteroid 5580 Sharidake or 1988 RP1, asteroid Sharidake, RP1 from 1998, the 5580th asteroid catalogued