9. Lunar Crewed Mission Profile MOON EARTH LLO 100 km Direct or Skip Entry ERO Up to 4 days LEO Loiter EDS Performs TLI on FD5 Nominal Water Landing Crew of 4 + 500 kg cargo Altair performs LOI 100 kg return payload Ares-1 Ascent Target 90 min. launch separation Orion 20.185 t at TLI Orion performs 3 Burn TEI up to 1,492 m/s
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16. Elements of Future Human Missions Beyond LEO Enabling Human Exploration Precursor Knowledge Needed Capabilities Destinations of Interest
17. The human-accessible solar system is richer than just the Moon and Mars Various program pathways through these destinations can build our capabilities Earth LEO ISS Moon Mars Earth-Moon L1 GEO Mars orbit Low lunar orbit Phobos Near Earth asteroids Sun-Earth L4,5 Sun-Mars L4,5 Sun-Earth L1 Sun-Earth L2 For Public Release Space radiation Landing, ascent, surface ops Deep space, long trips Remote EVA ops Gravity well Current capability
21. ⌠and begin trade-space discussions with potential International partners The Global Exploration Strategy Scientific Knowledge For Public Release Economic Expansion Public Engagement Exploration Preparation Global Partnerships
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Editor's Notes
Constellation is comprised of seven projects â Ares, Orion, Extravehicular Activities, Mission Operations, Ground Operations, Altair and Lunar Surface Systems
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