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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)
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 Space Shuttle external tank ... Empty weight: 58,500 lb (26,500 kg) ... to hold the weight of Space Shuttle Pathfinder at the U.S. Space & Rocket Center.
At the end of the Space Shuttle program the SCA was used to deliver the retired orbiters from the Kennedy Space Center to their museums. ... Empty weight: 318,000 lb ...
Vehicle Liftoff Mass Payload Mass to LEO Mass ratio Payload fraction Falcon 9 Block 5: 549,054 kg + 22,800 kg 22,800 kg 25.1 3.99% Proton-M: 705,000 kg + 23,000 kg
The RS-25 engine consists of pumps, valves, and other components working in concert to produce thrust. Fuel (liquid hydrogen) and oxidizer (liquid oxygen) from the Space Shuttle's external tank entered the orbiter at the umbilical disconnect valves and from there flowed through the orbiter's main propulsion system (MPS) feed lines; whereas in the Space Launch System (SLS), fuel and oxidizer ...
The Space Shuttle Solid Rocket Booster (SRB) was the first solid-propellant rocket to be used for primary propulsion on a vehicle used for human spaceflight. [1] A pair of them provided 85% of the Space Shuttle 's thrust at liftoff and for the first two minutes of ascent.
Soviet / Russian space station: LEO: Deorbited 2001: 1986–2001 Space Shuttle Atlantis STS-117: 122,683 kg (270,470 lb) Heaviest flight of the Space Shuttle with S3/S4 truss. LEO: Retired: 1985–2011 Space Shuttle Columbia STS-93: 122,534 kg (270,141 lb) Chandra X-ray Observatory, launch: LEO: Lost: 1981–2003 Space Shuttle Atlantis STS-115: ...