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The General Dynamics Nexus was proposed in the 1960s as a fully reusable successor to the Saturn V rocket, having the capacity of transporting up to 450–910 t (990,000–2,000,000 lb) to orbit. [63] [64] The American Saturn MLV family of rockets was proposed in 1965 by NASA as successors to the Saturn V rocket. [65]
U.S. space station; largest station orbited in one launch: LEO: Deorbited 1979: 1973–1979 Apollo 16 CSM+LM: 52,759 kg (116,314 lb) Heaviest spacecraft sent to lunar orbit. First mission to land in Lunar Highlands. Command module is on display in Alabama: Moon: Retired: 1972 Apollo 12 CSM+LM: 49,915 kg (110,044 lb) LEM landed at Sinus Medii a ...
A heavy-lift launch vehicle (HLV) is an orbital launch vehicle capable of lifting payloads between 20,000 to 50,000 kg (44,000 to 110,000 lb) (by NASA classification) or between 20,000 to 100,000 kilograms (44,000 to 220,000 lb) (by Russian classification) [1] into low Earth orbit (LEO). [2]
Number of rocket launches – the total number of launches, including failed launches; Heaviest rocket launched – total mass at lift-off; Highest achieved altitude – height in km above launch site (unless orbital) Notes – comments; Major/active spaceports are shown in bold.
List of Antares launches; List of Ariane launches; List of Atlas launches; List of Black Brant launches; List of Delta IV Heavy launches; List of Delta IV Medium launches; List of Electron rocket launches; List of failed Thor and Delta launches; List of Falcon 9 and Falcon Heavy launches; List of H-I and H-II launches; List of Launch Services ...
The 33 Raptor rocket engines affixed to the bottom of the Super Heavy rocket booster are seen firing as SpaceX launched its fifth flight test of Starship on October 13. - Spacex/UPI/Shutterstock
SpaceX has launched Starship, the biggest and most powerful rocket ever made, which then exploded. The rocket successfully left its launchpad in Texas, but the two pieces of the spacecraft failed ...
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.