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The Space Shuttle program used the HAL/S programming language. [11] The first microprocessor used was the 8088 and later the 80386. ... Space Shuttle design process.
The Space Shuttle orbiter is the ... the Space Shuttle orbiter resembled an airplane in its design, ... This was especially true in the interior of the payload bay. ...
Fish-eye lens view of the interior of Cupola with shutters closed Berthing operations within Cupola. The International Space Station Cupola was first conceived in 1987 by Space Station Man-Systems Architectural Control Manager Gary Kitmacher as a workstation for operating the station's Canadarm2 robotic arm, maneuvering vehicles outside the station, and observing and supporting spacewalks.
The Vehicle Assembly Building (originally the Vertical Assembly Building), or VAB, is a large building at NASA's Kennedy Space Center (KSC) in Florida, designed to assemble large pre-manufactured space vehicle components, such as the massive Saturn V, the Space Shuttle and the Space Launch System, and stack them vertically onto one of three mobile launcher platforms used by NASA.
During the design of the Space Shuttle, the Phase B proposals were not as cheap as the initial Phase A estimates indicated; Space Shuttle program manager Robert Thompson acknowledged that reducing cost-per-pound was not the primary objective of the further design phases, as other technical requirements could not be met with the reduced costs. [24]:
Spacelab art, with lab interior cutaway, 1981 Wubbo Ockels in the lab, 1985 Mercuric iodide crystals grown on Spacelab 3. Spacelab was a reusable laboratory developed by European Space Agency (ESA) and used on certain spaceflights flown by the Space Shuttle.
In the early 1990s, NASA engineers planning a crewed mission to Mars included a Shuttle-C design to launch six non reusable 80-ton segments to create two Mars ships in Earth orbit. After President George W. Bush called for the end of the Space Shuttle by 2010, these proposed configurations were put aside. [2] HLLV
The partial reusability of the Space Shuttle was one of the primary design requirements during its initial development. [65]: 164 The technical decisions that dictated the orbiter's return and re-use reduced the per-launch payload capabilities. The original intention was to compensate for this lower payload by lowering the per-launch costs and ...