Summary

| override_editor,  Advanced Automation for Space Missions… (1980)

“ In particular, this source could provide enormous masses of hydrogen throughout the Solar System. Given a means of collecting large fractions of the solar wind, eventually it may be possible to tap tiny portions of the 2×1027 ton mass of the Sun itself. Such a "star-centered" resource technology capability could decouple the extrasolar spread of humanity and its artifacts from the need for detailed knowledge of the star system of destination. ”
Source: Wikisource

| override_editor,  Advanced Automation for Space Missions… (1980)

“ The United States Space Transportation System (STS) , popularly known simply as the "Shuttle," is expected to establish approximately the same mass/year launching ratio during the 1980s at a cost of about $1000/kg to LEO. Energy represents only a small fraction of this expenditure. Perfectly efficient conversion of $0.05/kW-hr electricity into LEO orbital energy (about 10 kW-hr/kg) would cost roughly $0.50/kg for materials transport to orbit, a factor of 2000 less than near-term STS lift prices. Projected bulk transport versions of the STS may lower Earth-to-LEO expenses to $100/kg ”
Source: Wikisource

| override_editor,  Advanced Automation for Space Missions… (1980)

“ Other power sources which eventually may become accessible to mankind include the kinetic energy of the solar wind (1014 MW) ; differences in the orbital and rotational energies of the Sun, planets, moons, and asteroids (perhaps allowing payloads to move between these bodies) (Sheffield, 1979) ; and the thermodynamic energies associated with the differentiation of chemical elements in planetoids across the Solar System. ”
Source: Wikisource

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