• Thumbnail for Cryogenic rocket engine
    A cryogenic rocket engine is a rocket engine that uses a cryogenic fuel and oxidizer; that is, both its fuel and oxidizer are gases which have been liquefied...
    12 KB (645 words) - 23:30, 2 May 2025
  • Thumbnail for Liquid-propellant rocket
    RP-1, and a liquid oxidizer such as liquid oxygen. The engine may be a cryogenic rocket engine, where the fuel and oxidizer, such as hydrogen and oxygen...
    53 KB (6,608 words) - 04:23, 20 May 2025
  • Thumbnail for RL10
    RL10 (redirect from RL-10 (rocket engine))
    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...
    40 KB (2,895 words) - 13:54, 20 February 2025
  • virtually non-existent). Cryogenic fuels most often constitute liquefied gases such as liquid hydrogen. Some rocket engines use regenerative cooling,...
    11 KB (1,227 words) - 12:57, 17 June 2023
  • Thumbnail for SpaceX Raptor
    (FFSC) fuel cycle, and the first such engine to power a vehicle in flight. The engine is powered by cryogenic liquid methane and liquid oxygen, a combination...
    76 KB (6,611 words) - 04:06, 9 April 2025
  • Thumbnail for Centaur (rocket stage)
    com. Retrieved April 8, 2018. "Evolution of Pratt & Whitney's cryogenic rocket engine RL-10". Archived from the original on March 3, 2016. Retrieved...
    47 KB (4,402 words) - 07:29, 5 April 2025
  • Hindustan Aeronautics Limited (category Aircraft engine manufacturers of India)
    glider CE-7.5 — cryogenic rocket engine (in production, used on GSLV Mk.II Cryogenic upper stage CUS15) CE-20 — cryogenic rocket engine (in production...
    54 KB (4,453 words) - 17:55, 15 May 2025
  • Thumbnail for CE-7.5
    CE-7.5 (category Rocket engines of India)
    a cryogenic rocket engine developed by the Indian Space Research Organisation to power the upper stage of its GSLV Mk-2 launch vehicle. The engine was...
    9 KB (644 words) - 19:58, 22 March 2025
  • Thumbnail for CE-20
    CE-20 (category Rocket engines of India)
    The CE-20 is a cryogenic rocket engine developed by the Liquid Propulsion Systems Centre (LPSC), a subsidiary of the Indian Space Research Organisation...
    30 KB (2,701 words) - 05:45, 28 February 2025
  • Thumbnail for Gas-generator cycle
    Stangeland. "Turbopumps for Liquid Rocket Engines". Archived from the original on 2012-10-18. "Vulcain-2 Cryogenic Engine Passes First Test with New Nozzle...
    5 KB (485 words) - 03:51, 10 July 2024
  • Thumbnail for RS-25
    RS-25 (redirect from SSME (rocket engine))
    The RS-25, also known as the Space Shuttle Main Engine (SSME), is a liquid-fuel cryogenic rocket engine that was used on NASA's Space Shuttle and is used...
    107 KB (10,654 words) - 23:53, 6 May 2025
  • Thumbnail for Vulcain (rocket engine)
    liquid oxygen/liquid hydrogen cryogenic fuel. The new version for Ariane 6 is called Vulcain 2.1. The Vulcain rocket engine is named in French for Vulcan...
    16 KB (1,065 words) - 20:49, 6 March 2025
  • Thumbnail for Skyroot Aerospace
    Skyroot Aerospace (category Rocket engine manufacturers of India)
    privately developed Cryogenic Rocket engine". WION. 25 September 2020. Retrieved 25 September 2020. Kumar, Chethan (25 November 2021). "Cryogenic: India's first...
    30 KB (2,606 words) - 12:01, 20 April 2025
  • Thumbnail for Geosynchronous Satellite Launch Vehicle
    Vikas engine. It has a diameter of 2.8 m (9 ft 2 in). The third stage of the GSLV Mark II is propelled by the Indian CE-7.5 cryogenic rocket engine while...
    27 KB (1,937 words) - 15:26, 27 April 2025
  • Thumbnail for HG-3 (rocket engine)
    The HG-3 was a liquid-fuel cryogenic rocket engine which was designed for use on the upper stages of Saturn rockets in the post-Apollo era. Designed in...
    4 KB (272 words) - 07:38, 24 May 2024
  • Thumbnail for Vikas (rocket engine)
    VIKram Ambalal Sarabhai ) is a family of hypergolic liquid fuelled rocket engines conceptualized and designed by the Liquid Propulsion Systems Centre...
    9 KB (600 words) - 12:13, 30 March 2025
  • Thumbnail for LVM3
    LVM3 (redirect from Bahubali Rocket)
    2017). "Cryogenic rocket engine has been developed from scratch: Isro chief". LiveMint. Retrieved 30 May 2018. "India launches 'monster' rocket". BBC News...
    51 KB (4,181 words) - 21:56, 23 March 2025
  • Thumbnail for Liquid oxygen
    Liquid oxygen (redirect from Cryogenic LOX)
    consumption bases. Liquid oxygen is the most common cryogenic liquid oxidizer propellant for spacecraft rocket applications, usually in combination with liquid...
    13 KB (1,289 words) - 18:19, 26 April 2025
  • private startup) in India makes a breakthrough by 3d printing a cryogenic rocket engine from scratch. 3D printing began to be used in production versions...
    11 KB (1,092 words) - 17:24, 23 August 2024
  • Thumbnail for BE-3
    The BE-3 (Blue Engine 3) is a liquid hydrogen/liquid oxygen rocket engine developed by Blue Origin. The engine began development in the early 2010s and...
    18 KB (1,818 words) - 23:58, 24 April 2025
  • heated propellant would be fed through a conventional rocket nozzle to produce thrust. Its engine thrust would be directly related to the surface area...
    13 KB (1,547 words) - 10:38, 29 March 2025
  • Thumbnail for Rocket engine
    A rocket engine is a reaction engine, producing thrust in accordance with Newton's third law by ejecting reaction mass rearward, usually a high-speed jet...
    101 KB (11,722 words) - 04:15, 17 May 2025
  • Thumbnail for SCE-200
    SCE-200 (category Rocket engines of India)
    The SCE-200 (also referred as Semi-Cryogenic Engine-200) is a 2 MN thrust class liquid rocket engine, being developed to power Indian Space Research Organisation's...
    23 KB (2,014 words) - 13:22, 26 April 2025
  • Thumbnail for Delta Cryogenic Second Stage
    The Delta Cryogenic Second Stage (DCSS) is a family of cryogenic-fuelled rocket stages used on the Delta III, Delta IV, and on the Space Launch System...
    11 KB (764 words) - 02:23, 17 May 2025
  • Thumbnail for Vinci (rocket engine)
    Vinci is a restartable, cryogenic, liquid-propellant rocket engine that powers the upper stage of Ariane 6. While development began in 1998 for the planned...
    9 KB (878 words) - 17:51, 22 November 2024
  • Thumbnail for Demonstration Rocket for Agile Cislunar Operations
    compared with the specific impulse of the RL10, a liquid-fuel cryogenic rocket engine built in the United States by Aerojet Rocketdyne and which is used...
    25 KB (2,675 words) - 21:56, 19 May 2025
  • Thumbnail for V. Narayanan (engineer)
    V. Narayanan (born 14 May 1964) is an Indian cryogenic engineer and rocket scientist who is serving as Chairman of the Indian Space Research Organisation...
    26 KB (2,158 words) - 11:04, 25 April 2025
  • Thumbnail for J-2X
    J-2X (category Rocket engines using hydrogen propellant)
    The J-2X is a liquid-fueled cryogenic rocket engine that was planned for use on the Ares rockets of NASA's Constellation program, and later the Space Launch...
    13 KB (1,116 words) - 03:34, 24 October 2024
  • RD-0146 (category Rocket engines of Russia)
     'Rocket Engine 0146') is a liquid-fuel cryogenic rocket engine developed by KBKhA Kosberg in Voronezh, Russia. The RD-0146 is the first Russian rocket...
    10 KB (1,074 words) - 23:44, 3 January 2025
  • Thumbnail for Staged combustion cycle
    Lunar N1 rocket. The non-cryogenic N2O4/UDMH engine RD-253 using staged combustion was developed by Valentin Glushko circa 1963 for the Proton rocket. After...
    27 KB (2,731 words) - 16:01, 10 April 2025