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The Space Shuttle flight software that monitors and controls the Canadarm was developed in Houston, Texas, by the Federal Systems Division of IBM. Rockwell International 's Space Transportation Systems Division designed, developed, tested, and built the systems used to attach the Canadarm to the payload bay of the orbiter.
The testing process is extensive and rigorous; the software on the Shuttle is often considered to be among the most bug-free of operational systems. The laboratory contains a complete avionics mock-up of a Shuttle, designated OV-095. While only a skeleton of an orbiter, the electronics are identical in position and type to those used on the ...
Astronautix Space Shuttle article; NASA: The Space Shuttle Decision; INTRODUCTION TO FUTURE LAUNCH VEHICLE PLANS [1963–2001], M. Lindroos; 10 Space Shuttles which never flew (Lockheed Starclipper, Chrysler SERV, Phase B Shuttles, Rockwell C-1057, Shuttle C, Air Launched Sortie Vehicle (ALSV), Hermes, Buran, Shuttle II, Lockheed Martin ...
Following the project's preliminary design review in late 2019, [3] the vehicle's configuration was frozen. Possessing a height of 13.5 m and a diameter of 1.1 m, CALLISTO is a relatively compact rocket, a feat aided by its role as a demonstrator rather that an end product in and of itself. [ 5 ]
The IBM AP-101B CPU and I/O processor (right) and AP-101S (left) The IBM System/4 Pi is a family of avionics computers used, in various versions, on the F-15 Eagle fighter, E-3 Sentry AWACS, Harpoon Missile, NASA's Skylab, MOL, and the Space Shuttle, as well as other aircraft.
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.
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