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Capacity; Payload to Low Earth orbit; Mass: ... The Space Shuttle orbiter is the spaceplane component of the Space Shuttle, ... Empty weight: 171,961 lb (78,000 kg)
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 Space Shuttle external tank (ET) carried the propellant for the Space Shuttle Main Engines, and connected the orbiter vehicle with the solid rocket boosters. The ET was 47 m (153.8 ft) tall and 8.4 m (27.6 ft) in diameter, and contained separate tanks for liquid oxygen and liquid hydrogen.
The Shuttle Carrier Aircraft (SCA) are two extensively modified Boeing 747 airliners that NASA used to transport Space Shuttle orbiters. One (N905NA) is a 747-100 model, while the other (N911NA) is a short-range 747-100SR.
The Space Shuttle program was the fourth human spaceflight program carried out by the U.S. National Aeronautics and Space Administration (NASA), which accomplished routine transportation for Earth-to-orbit crew and cargo from 1981 to 2011.
Space Shuttle orbiter ... Space Shuttle: 8 [note 4] 37.24: 4.8 [note 5] 109,000: Fuel cells Runway landing (with one pilot and one drogue chute from mid-1990s) 12,500 ...
The orbiter was mounted relatively far forward for launch, its tail in-line with the booster's wings. The combined weight at launch would be about 2,030 tons. The orbiter would re-enter nose-high at an angle of about 60 degrees above horizontal, decelerating at a peak of 2G until it reached low subsonic speeds at 40,000 ft.
Space Shuttle Discovery (Orbiter Vehicle Designation: OV-103) is a retired American Space Shuttle orbiter. The spaceplane was one of the orbiters from NASA's Space Shuttle program and the third of five fully operational orbiters to be built. [2] Its first mission, STS-41-D, flew from August 30 to September 5, 1984.