NASA NTRS ยท 20120016901
DEPLOYTECH: Mars Sample Return Concept Study Delta Results
Abstract
Agenda for this presentation is Exhaust options to reduce the launch numbers from 3 to 2: (1) Mass Reduction of Max-C Rover, ACO Orbiter, and or ACO ERS (2) Eliminate Max-C Rover (3) Launch vehicle options (4) Solar Sail for all interplanetary propulsion, chemical for maneuvering Goal would be to: (1) Brainstorm any other alternatives we have not considered (2) Eliminate any of the options listed above (3) Go forward with a possible viable option that is identified.
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Russell, Tiffany. 2012-09-28. DEPLOYTECH: Mars Sample Return Concept Study Delta Results. https://ntrs.nasa.gov/citations/20120016901
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