A cross-disciplinary team of scientists and engineers applied expertise gained in Lunar Lander development to the conceptual design of a long-duration, deep space habitat for Near Earth Asteroid (NEA) missions. The design reference mission involved two launches to assemble 5-modules for a 380-day round trip mission carrying 4 crew members. The conceptual design process yielded a number of interesting debates, some of which could be significant design drivers in a detailed Deep Space Habitat (DSH) design. These issues included: Design to minimize crew radiation exposure, launch loads, communications challenges, docking system and hatch commonality, pointing and visibility, consumables, and design for contingency operations.
Issues and Design Drivers for Deep Space Habitats
2012
7 pages
Report
Keine Angabe
Englisch
Astrophysics , Deep space , Space habitats , Structural design , Microgravity , Long duration space flight , Extraterrestrial radiation , Life support systems , Potable water , Spacecrews , Solar electric propulsion , Extravehicular activity , Consumables(Spacecraft) , Near earth asteroid rendezvous mission , Low earth orbits
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