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Crew size Length (m) Diameter (m) Launch mass (kg) Power system Recovery method Payload (kg) ‡ First spaceflight § Last spaceflight Flights § Mercury USA: McDonnell Aircraft North American Aviation: LEO attained: Redstone MRLV Atlas LV-3B: 1: 3.34: 1.89: 1,400 Batteries Parachute splashdown (one drogue, one main) 1961 (1960) 1963: 6 (12 ...
Space Shuttle, Orion, Apollo CSM: Active Upper N 2 O 4 /MMH: Pressure-fed: 316 [1] 26,689 [1] ... Comparison of crewed space vehicles; Comparison of space station ...
NASA report JSC-03600 Apollo/Skylab ASTP and Shuttle Orbiter Major End Items, Final Report, March 1978; NASA report listing dispositions of all rockets and spacecraft used in the Apollo, Skylab, Apollo-Soyez Test Project and early shuttle missions, as of 1978. Apollo D-2 Proposal by General Electric, Encyclopedia Astronautica
Size; Height: 56.1 m (184 ft) ... The Space Shuttle is a retired, ... 1966, as the Apollo space program neared its design completion, NASA and the Air Force released ...
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 includes all upcoming rockets.
Space Shuttle orbiter: 122,683 kg (270,470 lb) Space Shuttle Atlantis on STS-117, the heaviest flight of the Space Shuttle. LEO: Retired: 1981–2011 Apollo CSM: 28,800 kg (63,493 lb) U.S. crewed spacecraft for entering lunar orbit: Moon: Retired: 1968–1975 (Block II) Orion Multi-Purpose Crew Vehicle: 26,520 kg (58,467 lb)
The original design of the heavy-lift Ares V, named in homage to the Saturn V, was 360 feet (110 m) in height and featured a core stage based on the Space Shuttle External Tank, with a diameter of 28 feet (8.4 m). It was to be powered by five RS-25 engines and two five-segment Space Shuttle Solid Rocket Boosters (SRBs).
FLO was cancelled during the design process along with the rest of the Space Exploration Initiative. [citation needed] The U.S. Ares V for the Constellation program was intended to reuse many elements of the Space Shuttle program, both on the ground and flight hardware, to save costs. The Ares V was designed to carry 188 t (414,000 lb) and was ...