Propulsion system options for a potential Sample Return Lander (SRL) for Mars
UNKNOWN
Preudhomme, Michael↗
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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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Low Temperature Rechargeable Li-ion Batteries for Potential Mars Sample Return and Small Robotic Missions
UNKNOWN
Bugga, Ratnakumar V.↗
A Mars Ascent Vehicle for Potential Mars Sample Return
This paper will cover the conceptual design of a Mars Ascent Vehicle (MAV) and efforts underway to raise the TRL at both the component and system levels. A system down select was executed resulting in a Hybrid Propulsion based Single Stage To Orbit (SSTO) MAV baseline architecture. This paper covers the Point of Departure design, as well as results of hardware developments that will be tested in several upcoming flight opportunities.
Dankanich, John↗