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  2. Comparison of orbital launcher families - Wikipedia

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

    A Saturn V rocket, one of the most powerful operational launch vehicles to date. This article compares different orbital launcher families (launchers which are significantly different from other members of the same 'family' have separate entries).

  3. Comparison of orbital launch systems - Wikipedia

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

    Falcon 9 Block 5, the most prolific active orbital launch system in the world. This comparison of orbital launch systems lists the attributes of all current and future individual rocket configurations designed to reach orbit. A first list contains rockets that are operational or have attempted an orbital flight attempt as of 2024; a second list ...

  4. Comparison of retired orbital launch systems - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_retired...

    This comparison of retired orbital launch systems lists the attributes of all retired individual rocket configurations designed to reach orbit. For a list of proposed rocket configurations or individual configurations currently being launched check out Comparison of Orbital Launch Systems .

  5. Comparison of orbital rocket engines - Wikipedia

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

    Comparison of orbital launch systems; Comparison of orbital launchers families; Comparison of crewed space vehicles; Comparison of space station cargo vehicles; Comparison of solid-fuelled orbital launch systems; List of space launch system designs; List of orbital launch systems

  6. Super heavy-lift launch vehicle - Wikipedia

    en.wikipedia.org/.../Super_heavy-lift_launch_vehicle

    A super heavy-lift launch vehicle is a rocket that can lift to low Earth orbit a "super heavy payload", which is defined as more than 50 metric tons (110,000 lb) [1] [2] by the United States and as more than 100 metric tons (220,000 lb) by Russia. [3]

  7. Comparison of retired orbital launch vehicles - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_retired...

    Vehicle Origin Manufacturer Height Mass to ... (kg) Reuse Launches (+ suborbital) Launch Sites Date of flight LEO GTO Other First Last Antares 110–130 United States: Orbital: 40.5-41.9 m 5,100 [1] 1,500 to SSO No 5 [1] MARS: 2013 2014 Antares 230 / 230+ United States: Northrop Grumman: 42.5 m 8,200 [1] 3,000 to SSO [a] No 13 MARS: 2016 2023 ...

  8. Comparison of crewed space vehicles - Wikipedia

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

    Launch system 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 ...

  9. Comparison of solid-fuelled orbital launch systems - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_solid...

    Vehicle Main stages Origin Manufacturer Height (meter) Diameter (meter) Weight (ton) Mass to... (kg) Maiden flight Retired Record Status Solid Liquid LEO Other orbit Ares I: 1 1 United States: Alliant Techsystems / Boeing: 94 5.5 25000 (2015) 0/0 Cancelled Athena I: 2 1 United States: Lockheed Martin: 1995 2001 3/4 Retired Athena Ic: 2 1 United ...