42 U.S.C. § 18322 — Space Launch System as follow-on launch vehicle to the Space Shuttle
submitted 16 years ago by Pub. L. 111-267 to r/title-42-THE-PUBLIC-HEALTH-AND-WELFARE · 451 words · no verdicts yet
NASA must build a new rocket, called the Space Launch System, to replace the Space Shuttle and reach beyond low-Earth orbit. At first it must lift 70 to 100 tons, growing to 130 tons or more once fully built out. It also has to carry astronauts and act as a backup for the Space Station.
(a) United States policy. It is U.S. policy for NASA* to build a Space Launch System* that replaces the Space Shuttle and can reach cis-lunar space* and regions beyond low-Earth orbit, so the U.S. can take part in the growing effort to use that part of space.
(b) Initiation of development. NASA must start developing this rocket right away. First, the Administrator* must begin development as soon as practical after October 11, 2010, meeting the minimum requirements in subsection (c). Second, to limit the cost of ending old contracts and to keep critical capabilities, the Administrator must, as much as practical, extend or change existing rocket-development contracts to meet those requirements — including contracts for ground-testing solid rocket motors, if needed to keep them available for the new rocket.
(c) Minimum capability requirements. The Space Launch System must meet minimum requirements. It must, at first, be able to lift payloads of 70 to 100 tons into low-Earth orbit, without an extra upper stage, to prepare for trips beyond low-Earth orbit. It must be able to carry an upper stage that raises its total lift capacity to 130 tons or more. It must be able to carry the multi-purpose crew vehicle. And it must be able to serve as a backup to deliver cargo or crew to the ISS* if commercial or partner vehicles can't. The rocket must also be flexible: designed from the start to carry a full payload of 130 tons or more, and built, as much as practical, so it can grow to carry even heavier loads later. Work on the core rocket and the upper stage should happen at the same time, as funding allows, with the core getting priority so it's ready to operate by December 31, 2016. The Administrator must keep, adapt, and grow critical skills in areas like solid and liquid engines, large fuel tanks, rocket propulsion, and ground testing, so the switch to this new rocket goes smoothly. Finally, the rocket must be able to evolve efficiently over time, adding new technology, competing sub-parts, and using commercial operations.
It is the policy of the United States that NASA* develop a Space Launch System* as a follow-on to the Space Shuttle that can access cis-lunar space* and the regions of space beyond low-Earth orbit in order to enable the United States to participate in global efforts to access and develop this increasingly strategic region.
The Administrator* shall, as soon as practicable after October 11, 2010, initiate development of a Space Launch System meeting the minimum capabilities requirements specified in subsection (c).
In order to limit NASA’s termination liability costs and support critical capabilities, the Administrator shall, to the extent practicable, extend or modify existing vehicle development and associated contracts necessary to meet the requirements in paragraph (1), including contracts for ground testing of solid rocket motors, if necessary, to ensure their availability for development of the Space Launch System.
The Space Launch System developed pursuant to subsection (b) shall be designed to have, at a minimum, the following:
The initial capability of the core elements, without an upper stage, of lifting payloads weighing between 70 tons and 100 tons into low-Earth orbit in preparation for transit for missions beyond low-Earth orbit.
The capability to carry an integrated upper Earth departure stage bringing the total lift capability of the Space Launch System to 130 tons or more.
The capability to lift the multipurpose crew vehicle.
The capability to serve as a backup system for supplying and supporting ISS* cargo requirements or crew delivery requirements not otherwise met by available commercial or partner-supplied vehicles.
The Space Launch System shall be designed from inception as a fully-integrated vehicle capable of carrying a total payload of 130 tons or more into low-Earth orbit in preparation for transit for missions beyond low-Earth orbit. The Space Launch System shall, to the extent practicable, incorporate capabilities for evolutionary growth to carry heavier payloads. Developmental work and testing of the core elements and the upper stage should proceed in parallel subject to appropriations. Priority should be placed on the core elements with the goal for operational capability for the core elements not later than December 31, 2016.
The Administrator shall ensure critical skills and capabilities are retained, modified, and developed, as appropriate, in areas related to solid and liquid engines, large diameter fuel tanks, rocket propulsion, and other ground test capabilities for an effective transition to the follow-on Space Launch System.
The capacity for efficient and timely evolution, including the incorporation of new technologies, competition of sub-elements, and commercial operations.
Source credit: (Pub. L. 111–267, title III, § 302, Oct. 11, 2010, 124 Stat. 2814.)
- 2010Enacted · Pub. L. 111-267 · 124 Stat. 2814
A history note hasn’t been published yet. The record shows enactment by Pub. L. 111-267 on 2010-10-11.
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