Overview

The design philosophy that will guide the design of early lunar habitats will be based on a compromise between the desired capabilities of the base and the economics of its development and implantation. Preferred design will be simple, make use of existing technologies, require the least amount of lunar surface preparation, and minimize crew activity. Three concepts for an initial habitat supporting a crew of four for 28 to 30 days are proposed. Two of these are based on using Space Station Freedom structural elements modified for use in a lunar-gravity environment. A third concept is proposed that is based on an earlier technology based on expandable modules. The expandable modules offer significant advantages in launch mass and packaged volume reductions. It appears feasible to design a transport spacecraft lander that, once landed, can serve as a habitat and a stand-off for supporting a regolith environmental shield. A permanent lunar base habitat supporting a crew of twelve for an indefinite period can be evolved by using multiple initial habitats. There appears to be no compelling need for an entirely different structure of larger volume and increased complexity of implantation. Hypes, W. D. and Butterfield, A. J. and King, C. B. and Qualls, G. D. and Davis, W. T. and Gould, M. J. and Nealy, J. E. and Simonsen, L. C. Langley Research Center HABITATS; LUNAR BASES; MODULES; SPACE STATIONS; SPACECREWS; VIKING LANDER SPACECRAFT; ECONOMICS; LAUNCHING; LUNAR SURFACE; REGOLITH...

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9781722975173

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