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  2. File:Simplified diagram of RS-25 rocket engine(SSME) , Jan ...

    en.wikipedia.org/wiki/File:Simplified_diagram_of...

    Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 or any later version published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts.

  3. 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.

  4. Sirius Space Services - Wikipedia

    en.wikipedia.org/wiki/Sirius_Space_Services

    Sirius Space Services is a rocket manufacturing company from Paris, Ile-de-France, France, founded in 2020. [1] The company is developing three rockets (launch vehicles): Sirius 1, Sirius 13, Sirius 15, which use STAR-1 engine. [2] [3] The launch facilities will be: Arnhem Space Centre (Australia) and Guiana Space Centre. [4]

  5. Rocketdyne LR-101 - Wikipedia

    en.wikipedia.org/wiki/Rocketdyne_LR-101

    Rocket engineer Robert C. Truax, who had led the initial design studies for the PGM-17 Thor missile had planned on propelling his 'X-3 Volksrocket' with four Rocketdyne LR-101 engines, but despite many test firings the rocket never left the ground.

  6. 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.

  7. Hyundai Sirius engine - Wikipedia

    en.wikipedia.org/wiki/Hyundai_Sirius_engine

    The 1.5 L (1,468 cc) Hyundai G4DJ engine was manufactured from 1989 to 1995 under license from Mitsubishi and was essentially a copy of the 8-valve version of the popular 4G15 powerplant, the engine's advertised power is 74–97 PS (54–71 kW; 73–96 hp) at 5,500 rpm with 12.6–14.3 kg⋅m (124–140 N⋅m; 91–103 lbf⋅ft) of torque at 3,000 rpm.

  8. RD-270 - Wikipedia

    en.wikipedia.org/wiki/RD-270

    In total, 27 test firings were performed with 22 engines, three engines were tested twice, and one of them was tested three times. [2] All works stopped later together with corresponding activities on the UR-700 project. The RD 270 was also considered for the R-56 rocket (although never formally adopted) until work on the design stopped in June ...

  9. RS-68 - Wikipedia

    en.wikipedia.org/wiki/RS-68

    The RS-68 (Rocket System-68) was a liquid-fuel rocket engine that used liquid hydrogen (LH 2) and liquid oxygen (LOX) as propellants in a gas-generator cycle. It was the largest hydrogen-fueled rocket engine ever flown. [3] Designed and manufactured in the United States by Rocketdyne (later Pratt & Whitney Rocketdyne and Aerojet Rocketdyne).