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  2. Non-rocket spacelaunch - Wikipedia

    en.wikipedia.org/wiki/Non-rocket_spacelaunch

    Although all space launches to date have been rockets, a number of alternatives to rockets have been proposed. [2] In some systems, such as a combination launch system, skyhook, rocket sled launch, rockoon, or air launch, a portion of the total delta-v may be provided, either directly or indirectly, by using rocket propulsion.

  3. Spacecraft propulsion - Wikipedia

    en.wikipedia.org/wiki/Spacecraft_propulsion

    For rocket-like propulsion systems, this is a function of mass fraction and exhaust velocity; mass fraction for rocket-like systems is usually limited by propulsion system weight and tankage weight. [ citation needed ] For a system to achieve this limit, the payload may need to be a negligible percentage of the vehicle, and so the practical ...

  4. Comparison of orbital launch systems - Wikipedia

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

    All launch vehicle propulsion systems employed to date have been chemical rockets falling into one of three main categories: Solid-propellant rockets or solid-fuel rockets have a motor that uses solid propellants, typically a mix of powdered fuel and oxidizer held together by a polymer binder and molded into the shape of a hollow cylinder. The ...

  5. Atmosphere-breathing electric propulsion - Wikipedia

    en.wikipedia.org/wiki/Atmosphere-breathing...

    Atmosphere-breathing electric propulsion, or air-breathing electric propulsion, shortly ABEP, [1] is a propulsion technology for spacecraft, which could allow thrust generation in low orbits without the need of on-board propellant, by using residual gases in the atmosphere as propellant. Atmosphere-breathing electric propulsion could make a new ...

  6. Theoretical spacecraft propulsion - Wikipedia

    en.wikipedia.org/wiki/Theoretical_spacecraft...

    The fission sail is a type of spacecraft propulsion proposed by Robert Forward that uses fission fragments to propel a large solar sail-like craft.It is similar in concept to the fission-fragment rocket in that the fission by-products are directly harnessed as working mass, and differs primarily in the way that the fragments are used for thrust.

  7. Aerojet Rocketdyne AR1 - Wikipedia

    en.wikipedia.org/wiki/Aerojet_Rocketdyne_AR1

    Aerojet Rocketdyne proposed in 2014 to "lobby the government to fund an all-new, U.S.-sourced rocket propulsion system." In June 2014, Aerojet initially projected it would cost under US$25 million per pair of engines, not including the up to US$1 billion estimated development cost to be funded by the government.

  8. College students break record for highest rocket launched by ...

    www.aol.com/news/college-students-break-record...

    We broke the world record and sent a rocket higher than any [amateur] ever has.” College students break record for highest rocket launched by amateurs at 89 miles above Earth Skip to main content

  9. Green Propellant Infusion Mission - Wikipedia

    en.wikipedia.org/wiki/Green_Propellant_Infusion...

    The GPIM system flew aboard the small Ball Configurable Platform 100 (BCP-100) spacecraft bus. [6] [11] Aerojet Rocketdyne was responsible for the development of the propulsion system payload, and the technology demonstration mission employed an Aerojet-developed advanced monopropellant payload module as the sole means of on-board propulsion. [10]