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  2. Space Launch System core stage - Wikipedia

    en.wikipedia.org/wiki/Space_Launch_System_core_stage

    The Space Launch System core stage, or simply core stage, is the main stage of the American Space Launch System (SLS) rocket, built by The Boeing Company in the NASA Michoud Assembly Facility. At 65 m (212 ft) tall and 8.4 m (27.6 ft) in diameter, the core stage contains approximately 987 t (2,177,000 lb) of its liquid hydrogen and liquid ...

  3. RS-25 - Wikipedia

    en.wikipedia.org/wiki/RS-25

    The RS-25 engine consists of pumps, valves, and other components working in concert to produce thrust. Fuel (liquid hydrogen) and oxidizer (liquid oxygen) from the Space Shuttle's external tank entered the orbiter at the umbilical disconnect valves and from there flowed through the orbiter's main propulsion system (MPS) feed lines; whereas in the Space Launch System (SLS), fuel and oxidizer ...

  4. List of spacecraft manufacturers - Wikipedia

    en.wikipedia.org/wiki/List_of_spacecraft...

    ID-1, ID-2, ID-3 and unnamed 2-stage rocket engine for DNLV solid rocket motor and liquid rocket engine: used on ID-1, ID-2 and DNLV rocket Borneo SubOrbitals: Malaysia hybrid rocket: used on yet-to-be-named rocket Apollo Fusion United States ACE, ACE Max Hall-effect thruster: To be used on Spaceflight, Inc.'s Sherpa-LTE space tug [46]

  5. Why Intuitive Machines Popped, but Rocket Lab and AST ... - AOL

    www.aol.com/why-intuitive-machines-popped-rocket...

    Volatility ran amok among space stocks Tuesday. Shares of lunar explorer Intuitive Machines (NASDAQ: LUNR) rocketed 35.6% through 3 p.m. ET, but rocket maker Rocket Lab (NASDAQ: RKLB) and satcom ...

  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. RL10 versions were produced for the Centaur upper stage of the Atlas V and the DCSS of the Delta IV

  7. Rocketdyne F-1 - Wikipedia

    en.wikipedia.org/wiki/Rocketdyne_F-1

    Larger solid-fuel engines exist, such as the Space Shuttle Solid Rocket Booster with a sea-level liftoff thrust of 2,800,000 lbf (12.45 MN) apiece. The Soviet (now Russian) RD-170 can develop more thrust than the F-1, at 1,630,000 lbf (7.25 MN) per engine at sea level, however, each engine uses four combustion chambers instead of one, to solve ...

  8. Rocket Fuel Inc. - Wikipedia

    en.wikipedia.org/wiki/Rocket_Fuel_Inc.

    Rocket Fuel acquired the New York-based ad tech company [x+1] in August 2014 for $230 million. [7] [8] [9] In 2017, the company was acquired by Sizmek, a private ad tech company owned by Vector Capital; one outcome of this was a retreat from public company status back to being a private company. [2] In November 2017, Sizmek retired the brand ...

  9. SpaceX Raptor - Wikipedia

    en.wikipedia.org/wiki/SpaceX_Raptor

    Raptor is a family of rocket engines developed and manufactured by SpaceX. It is the third rocket engine in history designed with a full-flow staged combustion (FFSC) fuel cycle, and the first such engine to power a vehicle in flight. [15] The engine is powered by cryogenic liquid methane and liquid oxygen, a combination known as methalox.