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The original intention was to compensate for this lower payload by lowering the per-launch costs and a high launch frequency. However, the actual costs of a Space Shuttle launch were higher than initially predicted, and the Space Shuttle did not fly the intended 24 missions per year as initially predicted by NASA. [54] [24]: III–489–490
[3] [4] Each Space Shuttle SRB provided a maximum 14.7 MN (3,300,000 lbf) thrust, [5] roughly double the most powerful single-combustion chamber liquid-propellant rocket engine ever flown, the Rocketdyne F-1. With a combined mass of about 1,180 metric tons (2,600,000 lb), they comprised over half the mass of the Shuttle stack at liftoff.
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 ...
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: ...
The Space Shuttle orbiter did not carry anti-collision lights, ... Empty weight: 171,961 lb (78,000 kg) Max takeoff weight: 242,508 lb (110,000 kg)
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.
Space Shuttle Endeavour (Orbiter Vehicle Designation: OV-105) is a retired orbiter from NASA's Space Shuttle program and the fifth and final operational Shuttle built. It embarked on its first mission, STS-49 , in May 1992 and its 25th and final mission, STS-134 , in May 2011.
The DC-3 was one of several early design proposals for the NASA Space Shuttle designed by Maxime Faget at the Manned Spacecraft Center (MSC) in Houston. It was nominally developed by North American Aviation (NAA), although it was a purely NASA-internal design.