National Aeronautics and Space Administration September 5, 2006 – Federal Register Recent Federal Regulation Documents

National Environmental Policy Act; Mars Science Laboratory Mission
Document Number: E6-14649
Type: Notice
Date: 2006-09-05
Agency: National Aeronautics and Space Administration, Agencies and Commissions
Pursuant to the National Environmental Policy Act of 1969, as amended, (NEPA) (42 U.S.C. 4321 et seq.), the Council on Environmental Quality Regulations for Implementing the Procedural Provisions of NEPA (40 CFR Parts 1500-1508), and NASA policy and procedures (14 CFR Part 1216 subpart 1216.3), NASA has prepared and issued a DEIS for the proposed MSL mission. The DEIS addresses the potential environmental impacts associated with implementing the mission. The purpose of this proposal is to explore the surface of Mars with a mobile science laboratory (rover). This environmental impact statement (EIS) is a tiered document (Tier 2 EIS) under NASA's Programmatic EIS for the Mars Exploration Program (MEP). The DEIS presents descriptions of the proposed MSL mission, spacecraft, and candidate launch vehicle; an overview of the affected environment at and near the launch site; and the potential environmental consequences associated with the Proposed Action and alternatives, including the No Action Alternative. The MSL mission is planned for launch during the September-November 2009 time period from Cape Canaveral Air Force Station (CCAFS), Florida, on an expendable launch vehicle. The arrival date at Mars would range from mid-July 2010 to not later than mid-October 2010, depending on the exact launch date and selected landing site, yet to be determined, on the surface of Mars. Using advanced instrumentation, the MSL rover would acquire significant, detailed information regarding the habitability of Mars from a scientifically promising location on the surface. The mission would also fulfill NASA's strategic technology goals of increasing the mass of science payloads delivered to the surface of Mars, expanding access to higher and lower latitudes, increasing precision landing capability, and increasing traverse capability (mobility) to distances on the order of several kilometers. The DEIS evaluates two alternatives in addition to the No Action Alternative. Under the Proposed Action (Alternative 1), the proposed MSL rover would utilize a radioisotope power system, a Multi-Mission Radioisotope Thermoelectric Generator (MMRTG), as its primary source of electrical power to operate and conduct science on the surface of Mars. Under Alternative 2, an MSL rover would utilize solar energy as its primary source of electrical power to operate and conduct science on the surface of Mars.
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