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  2. SpaceX Starship - Wikipedia

    en.wikipedia.org/wiki/SpaceX_Starship

    When stacked and fully fueled, Starship has a mass of approximately 5,000 t (11,000,000 lb), [c] a diameter of 9 m (30 ft) [12] and a height of 121.3 m (398 ft). [13] The rocket has been designed with the goal of being fully reusable to reduce launch costs; [14] it consists of the Super Heavy booster and the Starship upper stage [15] which are powered by Raptor and Raptor Vacuum engines.

  3. SpaceX Starship (spacecraft) - Wikipedia

    en.wikipedia.org/wiki/SpaceX_Starship_(spacecraft)

    Starship is a spacecraft and second stage [2] ... In May 2021, the SN15 prototype became the first full-size test spacecraft to take off and land successfully. [7]

  4. Starship - Wikipedia

    en.wikipedia.org/wiki/Starship

    Starship Dimensions (to-scale size comparisons) Starship Size Comparison Chart 1 (Dan Carlson, 13 July 2003) Starship Size Comparison Chart 2 (Dan Carlson, 30 October 2003) Starship Names (a Sci-Fi wiki article, outside Wikipedia)

  5. Starship will be bigger than the Great Pyramids, Elon ... - AOL

    www.aol.com/starship-bigger-great-pyramids-elon...

    At its current size, Starship can carry a payload of roughly 150 tonnes, according to SpaceX, while its internal volume provides enough space for up to 100 passengers.

  6. Super heavy-lift launch vehicle - Wikipedia

    en.wikipedia.org/wiki/Super_heavy-lift_launch...

    Starship is a two-stage-to-orbit fully reusable launch vehicle being privately developed by SpaceX, consisting of the Super Heavy booster as the first stage and a second stage, also called Starship. [ 22 ] [ 23 ] It is designed to be a long-duration cargo and passenger-carrying spacecraft . [ 24 ]

  7. List of heaviest spacecraft - Wikipedia

    en.wikipedia.org/wiki/List_of_heaviest_spacecraft

    1998– (at present size: 2021) Starship Ship 28 (V1) 200,000 kg (440,925 lb) [6] Mass is a rough estimate, including 100 tons of remaining propellant. Starship's first successful demonstration of reaching LEO [citation needed]. [6] Suborbital: Deorbited 2024 Mir: 129,700 kg (285,940 lb) Soviet / Russian space station: LEO: Deorbited 2001: 1986 ...

  8. Comparison of crewed space vehicles - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_crewed_space...

    Crew size Length (m) Diameter (m) Launch mass (kg) Power system Generated power (W) Recovery method First spaceflight § Last spaceflight Flights § SpaceShipOne USA: Scaled Composites: 112 km X Prize: White Knight Hybrid Motor: 1: 8.53 8.05 3,600 Batteries Runway landing 2004: 2004: 3 [note 22] X-15 USA: North American Aviation: 108 km ...

  9. 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.