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{{Short description|Joint US Air Force-NASA study to replace the Titan, Atlas and Space Shuttle rockets}}
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==Background==
[[File:Space Launch System (16525420976).jpg|alt=rocket ship|thumb|An artist's rendering of the 2010s [[Space Launch System]], which contains some design heritage from the ALS]]
The ALS was a joint USAF and NASA study from 1987 to 1990. It was an endeavour of the years following the [[Space Shuttle Challenger disaster
Although the project had a projected [[
The ALS program office differed from others in that it was the only one within the [[Air Force Space Command]]. The office was furnished with [[Macintosh|Apple Mac OS personal computers]] instead of the Command's usual [[Microsoft Windows#Early versions|Microsoft Windows]] systems{{Citation needed|date=July 2021}}. This was in part because NASA had already been using Apple computers. The program office pioneered what later became the [[Microsoft Project]]{{Citation needed|reason=The Wikipedia page for Project does not mention ALS or the USAF|date=July 2021}}.
== Aims ==
The ALS program was charged with deploying the space based elements of the [[Strategic Defense Initiative]] (SDI) program. Secondly, the ALS program was to find a way to transport many thousands of tons of equipment for the SDI into low Earth orbit at a cost less than $1,000 per kilogram. The usual cost was about $10,000 per kg.<ref>"ALS Contractors Concentrate on Expendable, Reusable Designs", Aerospace Daily, 20 June 1989 page 463</ref>
The program had three main contractors, each with an $800 million multi-year contract. They were Boeing Aerospace, Martin-Marietta, and General Dynamics. The ALS program budget was just under $2.5 billion.
By 1989, the [[Presidency of George H. W. Bush|Bush Administration]] had inherited a plan for the development of the Advanced Launch System that called for the Defense Acquisition Board to approve the advanced development of the system in early 1990, leading to a first flight in 1998 and a full operational capability in 2000.<ref>Wolfe, M.G. et al, "The Advanced Launch System." 40th International Astronautical Federation Congress, Malaga Spain, 8–14 October 1989, IAF Paper 89-229.</ref> This effort would lead to the development of a modular family of [[Launch vehicle|launch vehicles]], with a payload capacity to low Earth orbit ranging from 5,000 kilograms to 200,000 kilograms, that would replace existing expendable launch vehicles in the 2000-2005 time frame.<ref>Branscome, D.R., "The United States Space Transportation Survey," Proceedings of the 2nd European Aerospace Conference on Progress in Space Transportation, (European Space Agency, ESA SP-293, August 1989), pages 39-44.</ref>▼
== Progress ==
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==See also==
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