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The Space Shuttle orbiter is the spaceplane component of the Space Shuttle, ... Empty weight: 171,961 lb (78,000 kg) Max takeoff weight: 242,508 lb (110,000 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.
While on the pad, the two SRBs carried the entire weight of the external tank and orbiter and transmitted the weight load through their structure to the mobile launcher platform. Each booster had a liftoff thrust of approximately 12 meganewtons (2,800,000 pounds-force) at sea level, increasing shortly after liftoff to 14.7 MN (3,300,000 lbf). [5]
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.
The orbiter’s placement marks the first time a shuttle designed for space was assembled vertically outside of a NASA or Air Force facility. The space shuttle Endeavour is maneuvered into ...
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.
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