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  2. 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.

  3. Rocket Lab Electron - Wikipedia

    en.wikipedia.org/wiki/Rocket_Lab_Electron

    Its Rutherford engines are the first electric-pump-fed engine to power an orbital-class rocket. [17] Electron is often flown with a kickstage or Rocket Lab's Photon spacecraft. Although the rocket was designed to be expendable , Rocket Lab has recovered the first stage twice and is working towards the capability of reusing the booster. [ 18 ]

  4. Comparison of orbital rocket engines - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_orbital...

    Download as PDF; Printable version; In other projects ... This page is an incomplete list of orbital rocket engine data and specifications. ... full-flow: 350 [31 ...

  5. Rocket Lab - Wikipedia

    en.wikipedia.org/wiki/Rocket_Lab

    The Rutherford engine uses pumps driven by battery-powered electric motors rather than a gas generator, expander, or preburner. [107] The engine is fabricated largely by 3D printing , using electron beam melting , [ 108 ] whereby layers of metal powder are melted in a high vacuum by an electron beam. [ 109 ]

  6. Archimedes (rocket engine) - Wikipedia

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

    The engine is mostly 3D printed, [7] with some of the biggest 3D printers in the world. The rationale for the cycle change from the original gas generator was that they could not get the performance they needed through all the throttle points that a reusable rocket needs, without pushing the turbine temperature and other factors beyond their ...

  7. RL10 - Wikipedia

    en.wikipedia.org/wiki/RL10

    The RL10 is a liquid-fuel cryogenic rocket engine built in the United States by Aerojet Rocketdyne that burns cryogenic liquid hydrogen and liquid oxygen propellants. Modern versions produce up to 110 kN (24,729 lb f) of thrust per engine in vacuum.

  8. Electric-pump-fed engine - Wikipedia

    en.wikipedia.org/wiki/Electric-pump-fed_engine

    Electrical pumps had been used in the secondary propulsion system of the Agena upper stage vehicle. [ 1 ] As of December 2020, the only rocket engines to use electric propellant pump systems are the Rutherford engine, [ 2 ] ten of which power the Electron rocket, [ 2 ] and the Delphin engine, five of which power the first stage of Astra Space ...

  9. RD-120 - Wikipedia

    en.wikipedia.org/wiki/RD-120

    The RD-120 (Russian: Ракетный Двигатель-120, romanized: Raketnyy Dvigatel-120, lit. 'Rocket Engine 120', GRAU index: 11D123) is a liquid upper stage rocket engine burning RG-1 (refined kerosene) and LOX in an oxidizer rich staged combustion cycle with an O/F ratio of 2.6.