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I. Alternative Mission Concepts
Pages 5-10

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From page 5...
... Although it is technically feasible to go to the Moon and Mars without the intermediate step of establishing a permanent station in low Earth orbit (LEO) , most of the mission architectures under consideration employ a station for assembly of vehicles for travel beyond Earth, for storing fuel and supplies, and as a human transfer facility.
From page 6...
... THE NASA REPORT OF THE 90-DAY STUDY ON HUMAN EXPLORATION OF THE MOON AND MARS The NASA Report of the 90-Day Study provided descriptions of five reference approaches: Approach A is formulated to establish human presence on the Moon in 2001, and the Moon is used as a learning center to develop the capability to move on to Mars. An initial nuclear power unit and lunar oxygen production demonstration hardware are added in 2003 to reduce lunar logistics requirements.
From page 7...
... They employ unmanned robotic precursor missions, reusable transfer vehicles to lunar and Martian orbits, and excursion vehicles at surface bases. Each features sequential Moon and Mars programs, assumes zero gravity in transit to Mars and requires a decade or more of research on adaptability of humans to low or zero gravity, depends on aerobraking (using atmospheric drag to slow a vehicle for capture in the planetary gravity field)
From page 8...
... Human experience in space suggests that less EVA means safer missions, owing to the limited maneuverability and flexibility of astronauts in currently available space suits. Emphasis on teleoperations or more synergistic human/machine interactions can provide substitutes for extensive EVA But to facilitate a wide range of human activities in space, it seems desirable to develop an improved space suit for necessary EVA tasks.
From page 9...
... Further, The Great Exploration proposes no robotic precursor missions to learn more about the environments of the Moon or Mars or to identity safe or scientifically interesting landing sites. The committee believes The Great Exploration underestimates the many engineering and operational challenges involved in bringing its technical concepts to practical realization.
From page 10...
... Among other early architectures that might be considered are the NASA baseline concept, with the initial Mars base in orbit rather than on the surface and the NASA baseline with separate cargo and crew transport systems, the latter with high-speed, staged chemical propulsion and even Earth launch of lunar and Mars missions. The committee is convinced that other alternatives will arise as concept development proceeds.


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