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  2. 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

  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. Rocketdyne F-1 - Wikipedia

    en.wikipedia.org/wiki/Rocketdyne_F-1

    Another ten engines were installed on two ground-test Saturn Vs never intended to fly. The S-IC-T "All Systems Test Stage," a ground-test replica, is on display as the first stage of a complete Saturn V at the Kennedy Space Center in Florida. SA-500D, the Dynamic Test Vehicle, is on display at the U.S. Space and Rocket Center in Huntsville ...

  5. 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).

  6. To rival SpaceX’s Starship, ULA eyes Vulcan rocket upgrade

    www.aol.com/news/rival-spacex-starship-ula-eyes...

    ULA is aiming to fly eight Vulcan missions next year and 12 missions with Atlas V, Vulcan's retiring predecessor. Vulcan starts at a launch price of roughly $110 million - slightly over the base ...

  7. Comparison of crewed space vehicles - Wikipedia

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

    Saturn IB Saturn V: 3: 8.5: 3.91: 5,500 CM + 14,700 LM + 24,500 Service Module: Fuel cells Parachute splashdown (two drogues, three pilots, three mains) 1967 (1966) 1975: 15 (4) [note 3] Space Shuttle orbiter USA: Rockwell International: LEO: Space Shuttle: 8 [note 4] 37.24: 4.8 [note 5] 109,000: Fuel cells Runway landing (with one pilot and ...

  8. Vulcan Centaur - Wikipedia

    en.wikipedia.org/wiki/Vulcan_Centaur

    The following January, ULA was designing two versions of the Vulcan first stage; the BE-4 version has a 5.4 m (18 ft) diameter to support the use of the less dense methane fuel. [20] In late 2017, the upper stage was changed to the larger and heavier Centaur V, and the launch vehicle was renamed Vulcan Centaur. [41]

  9. Saturn V - Wikipedia

    en.wikipedia.org/wiki/Saturn_V

    The Saturn V reached 400 feet per second (120 m/s) at over 1 mile (1,600 m) in altitude. Much of the early portion of the flight was spent gaining altitude, with the required velocity coming later. The Saturn V broke the sound barrier at just over 1 minute at an altitude of between 3.45 and 4.6 miles (5.55 and 7.40 km). At this point, shock ...