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  2. Comparison of orbital launcher families - Wikipedia

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

    The article is organized into two tables: the first contains a list of currently active and under-development launcher families, while the second contains a list of retired launcher families. The related article " Comparison of orbital launch systems " lists each individual launcher system within any given launcher family, categorized by its ...

  3. Comparison of orbital launch systems - Wikipedia

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

    The following chart shows the number of launch systems developed in each country, and broken down by operational status. Rocket variants are not distinguished; i.e., the Atlas V series is only counted once for all its configurations 401–431, 501–551, 552, and N22.

  4. Scaled Composites Stratolaunch - Wikipedia

    en.wikipedia.org/wiki/Scaled_Composites_Stratolaunch

    In August 2014, all solid-fuel propulsion was selected, rather than liquid-fuel for the Orbital Sciences launcher. [12] In August 2015, 200,000 lb (91 t) of structure was assembled. [13] By June 2016, Scaled Composites had 300 people working on the project. [14] Virgin Orbit also planned to launch small satellites with the LauncherOne from a ...

  5. Cleveland Launcher XL Halo fairway woods, hybrids - AOL

    www.aol.com/news/cleveland-launcher-xl-halo...

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  6. Firefly Aerospace - Wikipedia

    en.wikipedia.org/wiki/Firefly_Aerospace

    Firefly Aerospace [1] [2] is an American private aerospace firm based in Cedar Park, Texas, that develops small-and medium-lift launch vehicles for commercial launches to orbit. [3]

  7. Small-lift launch vehicle - Wikipedia

    en.wikipedia.org/wiki/Small-lift_launch_vehicle

    A small-lift launch vehicle is a rocket orbital launch vehicle that is capable of lifting 2,000 kilograms (4,400 lb) or less (by NASA classification) or under 5,000 kilograms (11,000 lb) (by Roscosmos classification) [1] of payload into low Earth orbit (LEO).

  8. Rocket Lab Electron - Wikipedia

    en.wikipedia.org/wiki/Rocket_Lab_Electron

    Electron is a two-stage, partially reusable orbital launch vehicle developed by Rocket Lab, an American aerospace company with a wholly owned New Zealand subsidiary. [14] [15] Servicing the commercial small satellite launch market, [16] it is the third most launched small-lift launch vehicle in history.

  9. Power and Propulsion Element - Wikipedia

    en.wikipedia.org/wiki/Power_and_Propulsion_Element

    The PPE originally started development at the Jet Propulsion Laboratory as a part of the now cancelled Asteroid Redirect Mission, but is now led and managed by the NASA John H. Glenn Research Center, in Cleveland, Ohio. When ARM was cancelled, the solar electric propulsion was repurposed as the PPE for the Gateway.