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Results for “Mars exploration entry/descent/landing systems low-cost missions”

Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.

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NASA NTRS2002

Rough lander concept for Mars exploration

A new concept is proposed herein for small spacecraft that use a rough landing approach to enable a substantial reduction in delivery system complexity relative to previous soft landing systems.

Mars exploration entry/descent/landing systems low↗

NASA NTRS2002

Rough lander concept for Mars exploration

Explore the source record for details and available documents.

Mars exploration entry/descent/landing systems low↗