Robotic Explorer for Hypothesized Surfaces – CSU

INSTITUTION

Cleveland State University

CLASS

Cobalt Class (2019 – 2020)

STUDENT TEAM

Mark Ade
Nikola Blagojevic, Mechanical Engineering
Leah Bunnell, Mechanical Engineering and Physics
Rowan Myatt, Mechanical Engineering

ACADEMIC GUIDANCE

Dr. Michael Adams, Chair and Associate Professor of Engineering Technology, Cleveland State University

PROJECT DESCRIPTION

The Psyche mission is set to launch in 2022 and arrive at the asteroid in 2026. It is an orbiter mission and will not land on the surface. Instead, it will spend 21 months performing science operations from four staging orbits, which become successively closer. This will be NASA’s first space mission to a world likely made largely of metal, rather than rock or ice. The Psyche mission will take a giant step forward in our understanding of this mysterious world. It is possible to imagine, however, that after learning about Psyche from orbit, there may be scientists and engineers interested in proposing a subsequent mission to actually land on the asteroid to explore and sample its surface. Capstone teams are invited to take on that challenge!

Designing to the range of hypothesized surfaces that might be found at Psyche (and keeping in mind other constraints such as its gravity), the team is designing and prototyping a robotic explorer capable of efficiently traversing each of the hypothesized surfaces of Psyche and, ideally, able to adapt to each of them mid-traverse. Hypothesized surfaces may include: mostly flat metallic surface, flat metallic with metal and/or rocky debris, rough/high-relief metallic and/or rocky terrain, high-relief metallic crater walls.

This work was created in partial fulfillment of Cleveland State University Capstone Course “MCE 450”. The work is a result of the Psyche Student Collaborations component of NASA’s Psyche Mission (https://psyche.asu.edu). “Psyche: A Journey to a Metal World” [Contract number NNM16AA09C] is part of the NASA Discovery Program mission to solar system targets. Trade names and trademarks of ASU and NASA are used in this work for identification only. Their usage does not constitute an official endorsement, either expressed or implied, by Arizona State University or National Aeronautics and Space Administration. The content is solely the responsibility of the authors and does not necessarily represent the official views of ASU or NASA.