Flying on Mars starts with understanding Mars

A PhD project on Martian aerial robotics became a deeper question: not only how to fly on Mars, but which aircraft concepts make sense, where, why, and under what planetary conditions.
Flying on Mars starts with understanding Mars
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Mars has no shortage of aircraft ideas.

Over the years, researchers have proposed helicopters, fixed-wing aircraft, balloons, gliders, hoppers and hybrid concepts for exploring the red planet. When I began my PhD, I was also drawn to the technical challenge of designing an aerial robot for Mars. But as I went deeper into the literature, I found myself asking a different kind of question: which of these ideas actually make sense, where, and why?

That question became my way of putting some philosophy back into the Doctor of Philosophy.

From flying machines to planetary systems

NASA’s Ingenuity helicopter proved that powered flight on another planet is possible. That achievement changed the conversation around Mars exploration. But it also raised a larger question: what comes next?

Future Martian aerobots will need to do more than demonstrate flight. They may need to survey large regions, scout landing sites, reach cliffs and canyons, investigate difficult terrains, support rovers, and eventually assist human exploration. To do that, they cannot be designed only as aircraft. They need to be designed as planetary exploration systems.

That shift in thinking became the starting point for my Perspective article, “Mars planetary insights and design framework for future in-situ aerial robotic missions,” published in Communications Engineering.

Rather than beginning only with the aircraft, I wanted to begin with Mars itself.

Mars is not simply a distant runway waiting for a clever flying machine. It is a design environment shaped by thin air, low gravity, extreme temperature changes, dust storms, radiation, solar-energy limitations, complex terrain and strict landing constraints. Each of these factors changes what an aerobot can do, where it can operate, how long it can survive, and what kind of science it can realistically support.

The harder design question

One of the central ideas in the paper is that aerobot design should start with the planet and the mission, not only with the vehicle concept.

A rotorcraft, fixed-wing aircraft, balloon, hopper or hybrid vehicle may all be interesting. But each only becomes meaningful when matched to a specific scientific purpose, terrain type, atmospheric condition, energy strategy and deployment pathway.

This is where the paper brings together planetary science and aerospace engineering. Rovers and landers have transformed our understanding of Mars, but they are naturally limited by terrain, speed and landing safety. Aerobots could extend exploration beyond these limits by enabling rapid regional surveys, accessing high-priority sites beyond rover reach, and supporting future human exploration through environmental reconnaissance.

To support this thinking, the article introduces the Mars Aerobot Design Thinking Matrix. In simple terms, the matrix is a way to connect scientific goals with engineering decisions. It asks questions such as:

What is the mission trying to achieve?
What terrain must be reached?
What atmospheric conditions will the vehicle face?
What power source is realistic?
How will the aerobot be delivered and deployed?
What risks must be controlled before the system can become scientifically useful?

Diagram showing a Mars aerobot design framework that links mission objectives, environmental conditions, vehicle configuration, energy strategy, deployment method and operational requirements for future aerial robotic missions on Mars.
Figure:  The Mars Aerobot Design Thinking Matrix, a systems-level framework for connecting Mars mission goals, environmental constraints and aerobot design decisions.

For me, this was the most important part of the work. The paper is not only a catalogue of aircraft concepts. It is an attempt to place those concepts into a more systematic design logic, where mission purpose, planetary context and engineering feasibility are considered together.

One reviewer captured this aim very well:

“The paper is novel in that it brings all the issues together in one place and offers a structured ‘systems design’ approach to thinking about the design problem. The paper will be of value to any researcher embarking on Mars aerobot design... Overall, this is a very good paper which introduces the reader to many of the key issues involved in Mars aerobot design - no easy task. ”

What I learned behind the paper

Writing this article changed how I understood my own PhD journey.

At first, I thought the core challenge was technical: how to design a flying robot for Mars. But the deeper question was both philosophical and practical: why should such a system exist, what scientific gap would it fill, and how can it be designed honestly around the planet it must operate on?

That is why this paper became more than a review for me. It became a reflection on how engineering ideas gain meaning when they are connected to place, purpose and context.

Ingenuity opened the door to powered flight on another world. The next generation of Martian aerobots will need to go further: not only flying, but flying with scientific purpose, operational resilience and design logic grounded in Mars itself.

I am grateful to my co-authors Leonard Felicetti and Dmitry Ignatyev for their collaboration, and to the reviewers for their guidance, constructive feedback and encouragement throughout the publication process.

Read the article here:
https://doi.org/10.1038/s44172-026-00647-y

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Aerospace Technology and Astronautics
Technology and Engineering > Mechanical Engineering > Vehicle Engineering > Aerospace Technology and Astronautics
Planetary Science
Physical Sciences > Physics and Astronomy > Astronomy, Cosmology and Space Sciences > Planetary Science
Robotic Engineering
Technology and Engineering > Electrical and Electronic Engineering > Control, Robotics, Automation > Robotic Engineering
Engineering Design
Technology and Engineering > Mechanical Engineering > Engineering Design
Vehicle Engineering
Technology and Engineering > Mechanical Engineering > Vehicle Engineering
Engineering Mechanics
Technology and Engineering > Mathematical and Computational Engineering Applications > Engineering Mechanics

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