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  2. Rocket propellant - Wikipedia

    en.wikipedia.org/wiki/Rocket_propellant

    Solid rockets use propellant in the solid phase, liquid fuel rockets use propellant in the liquid phase, gas fuel rockets use propellant in the gas phase, and hybrid rockets use a combination of solid and liquid or gaseous propellants. In the case of solid rocket motors, the fuel and oxidizer are combined when the motor is cast.

  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

  4. Hybrid-propellant rocket - Wikipedia

    en.wikipedia.org/wiki/Hybrid-propellant_rocket

    Hybrid rocket propulsion system conceptual overview. In its simplest form, a hybrid rocket consists of a pressure vessel (tank) containing the liquid oxidizer, the combustion chamber containing the solid propellant, and a mechanical device separating the two. When thrust is desired, a suitable ignition source is introduced in the combustion ...

  5. Hybrid rocket fuel regression - Wikipedia

    en.wikipedia.org/wiki/Hybrid_Rocket_Fuel_Regression

    Hybrid rocket fuel regression refers to the process by which the fuel grain of a hybrid-propellant rocket is converted from a solid to a gas that is combusted. It encompasses the regression rate, the distance that the fuel surface recedes over a given time, as well as the burn area, the surface area that is being eroded at a given moment.

  6. Rocket engine - Wikipedia

    en.wikipedia.org/wiki/Rocket_engine

    RS-68 being tested at NASA's Stennis Space Center Viking 5C rocket engine used on Ariane 1 through Ariane 4. 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 of high-temperature gas produced by the combustion of rocket propellants stored inside the rocket.

  7. High-test peroxide - Wikipedia

    en.wikipedia.org/wiki/High-test_peroxide

    HTP is used on ILR-33 AMBER [7] and Nucleus [8] suborbital rockets. HTP was planned for use in an attempt to break the land speed record with the Bloodhound SSC car, aiming to reach over 1,000 miles per hour (1,600 km/h). HTP would have been the oxidiser for the hybrid fuel rocket, reacting with the solid fuel hydroxyl-terminated polybutadiene ...

  8. Gas vs. Electric vs. Hybrid: Find Out Which Is Really the ...

    www.aol.com/gas-vs-electric-vs-hybrid-143021118.html

    Car insurance costs jumped 26% this year, making it more important than ever to compare quotes from the best car insurance companies. Electric vehicles can be the most expensive to own Average ...

  9. Comparison of orbital launch systems - Wikipedia

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

    Hybrid-propellant rockets use a combination of solid and liquid propellant, typically involving a liquid oxidizer being pumped through a hollow cylinder of solid fuel. All current spacecraft use conventional chemical rockets (solid-fuel or liquid bipropellant) for launch, though some [note 3] have used air-breathing engines on their first stage ...