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Regolith - Rocket Plume Interaction: In situ measurements to enable multiple landings at the same Planetary Surface Site

Completed TRL 4 (started at 2, targeting 4)

Description

This project proposes to develop a prototype sensor package to measure the speed and direction of debris lofted by planetary lander terminal descent engines. The ultimate goal is to develop the technology for a package small enough to be flown as a secondary payload on future robotic landers. Because the physics of ejecta flight is different on the Moon and Mars, a significant innovative aspect of this project is development of technology for a sensor package that could gather needed data at both locations.

Benefits

NASA's future human exploration plans call for repeated landings of large vehicles at a single surface site. Such an approach raises the possibility of lander engines creating debris that could harm the lander and surface infrastructure. In-situ ejecta data will be needed to assist in lander design and surface site layout. STMD Technology Maturation support opportunities would be valuable in taking results from commercial-off-the-shelf (COTS) based prototype hardware and experience gained from using this prototype hardware in ground test stands to develop flight hardware of significantly reduced mass and power usage such that it can be on small robotic landers, such as the smaller range of proposed Commercial Lunar Payload Service (CLPS) landers or Mars landers of the sized used for the recent Insight mission.

Details

Technology areaEntry, Descent, and Landing > Vehicle Systems > Integrated Modeling and Simulation for EDL
ProgramCenter Innovation Fund: JSC CIF (JSC CIF)
Lead organizationJohnson Space Center, Houston, TX
Start date2018-10-01
End date2019-09-30

Project contacts

Listed on TechPort itself — the most direct way to ask about this specific project.

How to get involved

This is early/mid-stage (TRL 4) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.

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