Publication Date:
2019-07-13
Description:
Develop two evolutionary rigid vehicle concepts to deliver human-scale payloads (20 metric tons) to the surface of Mars: Capsule; Lifting body, mid-range lift-to-drag ratio (Mid L/D). Determine vehicle configurations for various mission flight phases. Determine vehicle performance: Integrated system mass; Ability to meet landing constraints; Payload packaging and surface access. Provide technology investment recommendations to NASAs Space Technology Mission Directorate.
Keywords:
Lunar and Planetary Science and Exploration; Spacecraft Design, Testing and Performance
Type:
MSFC-E-DAA-TN61432
,
Space and Astronautics Forum (AIAA SPACE Forum 2018); Sep 17, 2018 - Sep 19, 2018; Orlando, FL; United States
Format:
application/pdf
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