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  2. Reaction Motors XLR11 - Wikipedia

    en.wikipedia.org/wiki/Reaction_Motors_XLR11

    The XLR11, company designation RMI 6000C4, was the first liquid-propellant rocket engine developed in the United States for use in aircraft. It was designed and built by Reaction Motors Inc. , and used ethyl alcohol and liquid oxygen as propellants to generate a maximum thrust of 6,000 lbf (27 kN).

  3. Liquid rocket propellant - Wikipedia

    en.wikipedia.org/wiki/Liquid_rocket_propellant

    About 170 different propellants made of liquid fuel have been tested, excluding minor changes to a specific propellant such as propellant additives, corrosion inhibitors, or stabilizers. In the U.S. alone at least 25 different propellant combinations have been flown. [2] Many factors go into choosing a propellant for a liquid-propellant rocket ...

  4. 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

  5. RP-1 - Wikipedia

    en.wikipedia.org/wiki/RP-1

    RP-1 (Rocket Propellant-1 or Refined Petroleum-1) and similar fuels like RG-1 and T-1 are highly refined kerosene formulations used as rocket fuel. Liquid-fueled rockets that use RP-1 as fuel are known as kerolox rockets. In their engines, RP-1 is atomized, mixed with liquid oxygen (LOX), and ignited to produce thrust.

  6. Liquid-propellant rocket - Wikipedia

    en.wikipedia.org/wiki/Liquid-propellant_rocket

    A liquid-propellant rocket or liquid rocket uses a rocket engine burning liquid propellants. (Alternate approaches use gaseous or solid propellants.) Liquids are desirable propellants because they have reasonably high density and their combustion products have high specific impulse (I sp). This allows the volume of the propellant tanks to be ...

  7. Cryogenic fuel - Wikipedia

    en.wikipedia.org/wiki/Cryogenic_fuel

    Cryogenic fuels are fuels that require storage at extremely low temperatures in order to maintain them in a liquid state. These fuels are used in machinery that operates in space (e.g. rockets and satellites) where ordinary fuel cannot be used, due to the very low temperatures often encountered in space, and the absence of an environment that supports combustion (on Earth, oxygen is abundant ...

  8. Where are the wildfires in Texas right now? Map shows ... - AOL

    www.aol.com/where-wildfires-texas-now-map...

    The Pantex Plant, a nuclear weapon ... Where wildfires are burning in Texas right now. Tracking the fires: Texas fires map: Track wildfires as Smokehouse Creek blaze engulfs 500,000 acres.

  9. Titan IV - Wikipedia

    en.wikipedia.org/wiki/Titan_IV

    Power Plant: Stage 0 consisted of two solid-rocket motors. Stage 1 used an LR87-AJ-11 liquid-propellant rocket engine. Stage 2 used the LR91-AJ-11 liquid-propellant engine. Optional upper stages included the Centaur and Inertial Upper Stage. Guidance System: A ring laser gyro guidance system manufactured by Honeywell. Thrust: