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Future Lunar exploration plans will call for delivery of significant amounts of cargo to provide for crew habitation, surface transportation, and scientific exploration activities. Minimization of costly surface based Infrastructure is In large part directly related to the design of the cargo delivery / landing craft. this study focused on evaluating Lunar lander concepts from a logistical oriented perspective, and outlines the approach used In the development of a preferred configuration, sets forth the benefits derived from Its utilization and describes the missions and systems considered. Results indicate that only direct-to-surface downloading of payloads provides for unassisted cargo removal operations imperative to efficient and low risk site buildup, including the emplacement of Space Station derivative surface habitat modules, immediate cargo Jettison for both descent abort and emergency surface ascent essential to piloted missions carrying cargo, and short habitat egress/ingress paths necessary to productive surface work tours for crew members carrying hand held experiments, tools and other bulky articles. Accommodating cargo in a position underneath the vehicles structural frame, landing craft described herein eliminate altogether the necessity for dedicated surface based off-loading vehicles, the operations and maintenance associated with their operation, and the precipitous ladder climbs to and from the surface that are inherent to traditional designs. Parametric evaluations illustrate performance and mass variation with respect to mission requirements.

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This page is a summary of: Logistics impacts on lunar and Mars lander design, November 1991, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.1991-4139.
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