Skip Navigation
SBIR/STTR

Robotic ISRU Construction of Planetary Landing and Launch Pad, Phase I

Completed Technology Project

Project Introduction

The Apollo 15 Lunar Module rocket plume excavated regolith which sandblasted at speeds in excess of 1000 m/s the Surveyor 2 lander 200 m away. A Curiosity rover instrument was permanently damaged during SkyCrane landing on Mars. Any future human surface missions to planetary bodies covered in regolith (e.g. Mars, Moon) would need to address ejecta created during landing or takeoff. The intent of this project is to develop a fully robotic system for building landing pads on planetary bodies. The system will excavate in-situ regolith, sort rocks according to needed particle sizes, and layout a carefully designed landing/launch pad apron to lock in the small regolith particles. To that extent, Honeybee/MTU propose to design and build a robotic tool to perform the following 3 actions: Pick up or excavate rocks, sort the rocks in three size ranges, and deposit said rocks in three layers with the purpose to stabilize the fine regolith in the secondary apron zone of Lunar and Martian landing pads for repeated landings and take-offs. More »

Anticipated Benefits

Primary U.S. Work Locations and Key Partners

Share this Project

Organizational Responsibility

Project Management

Project Duration

Technology Maturity (TRL)

Technology Areas

Light bulb

Suggest an Edit

Recommend changes and additions to this project record.
^