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  2. 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]

  3. Comparison of orbital rocket engines - Wikipedia

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

    Engine Origin Designer Vehicle Status Use Propellant Power cycle Specific impulse (s) [a] Thrust (N) [a] Chamber pressure (bar) Mass (kg) Thrust: weight ratio [b] Oxidiser: fuel ratio AJ-10-190 USA: Aerojet: Space Shuttle, Orion, Apollo CSM: Active Upper N 2 O 4 /MMH: Pressure-fed: 316 [1] 26,689 [1] 8.62 [1] 118 [1] 23.08: Archimedes New ...

  4. Mitsubishi Sirius engine - Wikipedia

    en.wikipedia.org/wiki/Mitsubishi_Sirius_engine

    A UK-market Evo known as the FQ400 had a 400 bhp (298 kW; 406 PS) version of the Sirius, making it the most powerful car ever sold by Mitsubishi. The 4D6 diesel engines supplemented the larger 4D5. Bore pitch is 93 mm.

  5. Firefly Aerospace - Wikipedia

    en.wikipedia.org/wiki/Firefly_Aerospace

    Reaver is an expendable rocket engine designed for use on Firefly's Alpha rocket. It produces 184 kilonewtons (41,000 lb f ) of thrust and a specific impulse of 295.6 seconds (2.899 km/s). It is powered by RP-1 and liquid oxygen as its fuel and oxidizer, respectively.

  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. Template:Rocket engines - Wikipedia

    en.wikipedia.org/wiki/Template:Rocket_engines

    The engine has an article of at least Start class. The engine has been test fired, at least at the flight component or sub-scale level. The intent is for the rocket to be used in an orbital launch vehicle in the next five years. Examples: SCE-200 or Raptor (rocket engine) as of 2016. Option B. The engine has an article of at least Start class.

  8. 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.

  9. 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.