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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 ...
The American Saturn MLV family of rockets was proposed in 1965 by NASA as successors to the Saturn V rocket. [64] 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 [ 65 ] Nova was cancelled in 1964 and had reusable ...
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
The ICPS used on the Artemis I mission was powered by a single RL10B-2 engine, while the ICPS for Artemis II and Artemis III will use the RL10C-2 variant. [ 44 ] [ 45 ] [ 46 ] Block 1 is intended to be capable of lifting 209,000 lb (95 t) to low Earth orbit (LEO) in this configuration, including the weight of the ICPS as part of the payload. [ 47 ]
The C-5 was confirmed as NASA's choice for the Apollo program in early 1962, and was named the Saturn V. [31] [32] The C-1 became the Saturn I and C-1B became Saturn IB. [32] Von Braun headed a team at the MSFC to build a vehicle capable of launching a crewed spacecraft to the Moon. [ 33 ]
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 ...
The Ares IV concept combines an Ares I upper stage on top of an Ares V. [23] Specifically, the vehicle would consist of the liquid-fueled core stage from the Ares V design, two five-segment solid rocket boosters, and the liquid-fueled upper stage from the Ares I, as described by NASA in January 2007. The Ares IV would be a combined 367 ft (112 ...
The Vehicle Assembly Building (originally the Vertical Assembly Building), or VAB, is a large building at NASA's Kennedy Space Center (KSC) in Florida, designed to assemble large pre-manufactured space vehicle components, such as the massive Saturn V, the Space Shuttle and the Space Launch System, and stack them vertically onto one of three mobile launcher platforms used by NASA.