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The American Saturn MLV family of rockets was proposed in 1965 by NASA as successors to the Saturn V rocket. [69] It would have been able to carry up to 160,880 kg (354,680 lb) to low Earth orbit. The Nova designs were also studied by NASA before the agency chose the Saturn V in the early 1960s [ 70 ] Nova was cancelled in 1964 and had reusable ...
The following are a list of spacecraft with a mass greater than 8,000 kg (17,637 lb), or the top three to any other orbit including a planetary orbit, or the top three of a specific category of vehicle, or the heaviest vehicle from a specific nation. All numbers listed below for satellites use their mass at launch, if not otherwise stated.
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) [16] and a height of 121.3 m (398 ft). [17] The rocket has been designed with the goal of being fully reusable to reduce launch costs; [18] it consists of the Super Heavy booster and the Starship upper stage [19] which are powered by Raptor and Raptor Vacuum engines.
The uncrewed Starship spacecraft launched aboard the most powerful rocket ever built on Saturday morning, but both were lost shortly after liftoff.. The Super Heavy rocket booster ignited its 33 ...
Rocket 3 (2020–2022) LauncherOne (2020–2023) Firefly Alpha (2021–present) Space Launch System (2022–present) RS1 (2023–present) Terran 1 (2023) SpaceX Starship (2023–present) Vulcan Centaur (2024–present) New Glenn (Under development, expected 2024) Rocket 4 (Under development, expected 2025) Neutron (Under development, expected 2025)
SpaceX's next-generation Starship spacecraft atop its powerful Super Heavy rocket is launched on its sixth test at the company's Boca Chica launch pad in Brownsville, Texas, U.S., November 19, 2024.
SpaceX has launched its Starship aircraft, the world’s most powerful rocket, with partial success. The two-stage rocketship blasted off from the Elon Musk-owned company’s Starbase launch site ...
Falcon Heavy has the second highest lift capability of any operational rocket, with a payload of 63,800 kg (140,700 lb) to low Earth orbit, 26,700 kg (58,900 lb) to Geostationary Transfer Orbit, and 16,800 kg (37,000 lb) to trans-Mars injection. [66] The rocket was designed to meet or exceed all current requirements of human rating.