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Mars Electric Reusable Flyer, Year 1

Completed TRL 3 (started at 1, targeting 3)

Description

Research will include further development of the the vehicle configuration. It will continue the current Autonomy Incubator effort of developing visual odometry algorithms and Simultaneous Linearization and Mapping (SLAM) algorithms for specific application to Mars navigation in canyons and lava tubes. This effort will include wind tunnel testing in the LaRC TDT at Mars flight Reynolds number conditions to validate the design in Mars flight conditions. In addition, vacuum chamber tests and a balloon drop from high altitude (approximately 100k feet) will be performed to verify vehicle controlability and performance in Mars atmosphere density conditions.

Benefits

Goal to mature the technology so it can be a payload on the Mars 2020 mission. Flight on Mars would allow better navigation scouting for the ground rover, identification of high-value science targets, and gathering of ultra-high definition imagery for science purposes and the future human missions.

Details

ProgramCenter Innovation Fund: LaRC CIF (LaRC CIF)
Lead organizationLangley Research Center, Hampton, VA
Start date2015-10-01
End date2016-09-30

Project contacts

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