How To Aerobrake a Mission To Uranus On the Cheap

By Andy Tomaswick - May 12, 2025 at 7:31 AM UTC | Missions
Design of a proposed UOP mission, including an aerobrake at Uranus itself. Credit - Gomez-Delrio et al.
Design of a proposed UOP mission, including an aerobrake at Uranus itself. Credit - Gomez-Delrio et al.

Getting a probe to the Icy Giant planets takes some time - a journey to Uranus could take as long as 13 years, even with a gravity assist from Jupiter. However, several ideas are in the works to speed up that process, especially given the increased interest in sending a probe their way. One of those ideas is to use an aerocapture system to slow a probe down once it reaches its intended target. A new paper from Andrew Gomez-Delrio and their co-authors at NASA's Langley Research Center describes how a proposed Uranus Orbiter and Probe (UOP) mission could utilize the same aerocapture technology that Curiosity used to dramatically improve both the speed and payload capacity of the mission.

Using an aerocapture system for an Icy Giant mission has several advantages. First, as mentioned above, it can dramatically decrease the necessary travel time to get there. Some estimates suggest the travel time could be as much as halved, but at the very least, it would shave years off the journey. Second, it increases the percentage of payload that can be utilized for the primary mission rather than as propulsive fuel to get there. The third advantage is the propulsion system's decrease in size and complexity.

All those advantages make an aerocapture system sound like a good addition to any mission to Uranus, so what's the catch? Developing such a system would typically take years and cost millions of dollars. But, according to the paper, there's no need for that - project engineers could just slightly modify the aerocapture system used to successfully deliver the Mars Science Laboratory - better known now as Curiosity - to the surface of the red planet.

An old video from NASA explains why aerobraking is so critical.
Credit - NASA Video YouTube Channel

Despite the seemingly very different nature of the two missions, the aerocapture system could be essentially the same. Formally, it is known as the Thermal Protective System (TPS). Its main component is Conformal Phenolic Impregnated Carbon Ablator (CPICA), a material commonly used in heat shields due to its low density and thermal conductivity. Despite being very porous, it is one of the best materials for protecting spacecraft from the heat they suffer upon reentry into a planet's atmosphere.

Or, in this case, as it passes through a planet's atmosphere. The intention with the Uranus probe isn't to stop in the planet's atmosphere but to travel through it, using its slowing effect on the spacecraft as a type of brake. In a typical scenario, the TPS would either come down with the spacecraft itself once it had been sufficiently slowed or be jettisoned as the spacecraft makes its way onto the surface of another planet. In the UOP's case, it would jettison the TPS before settling into a stable orbit around its target planet.

But the aerocapture system is only one part of the overall thermal management of the spacecraft, and the paper from Dr. Gomez-Delrio considers several other systems, such as fancy types of insulation and constant conduction heat pipes running heat from the several radioisotope thermal generator power systems out to the rest of the mission hardware. The paper also provides a detailed analysis of how these systems perform at different mission stages, such as a Venus flyby and its "hibernation cruise".

NASA Technologist explains the concept of aerobraking.
Credit - GalacticLab YouTube Channel

As with all such missions, weight is a major defining feature, and an aerocapture system would save significant amounts of weight in the form of less fuel and unneeded external fuel tanks. This weight savings also allows for other vehicle configurations, including some that would enable the UOP to collect data during its cruise phase or release multiple Small Next-Generation Atmospheric Probes (SNAPs).

There's still a long way to go before UOP, as it still lacks funding despite being the highest-priority flagship mission of the latest Planetary Decadal Survey. Given the general lack of funding, there is a decent chance the mission itself might never get off the ground. But, in the meantime, projects like the one that resulted in this paper, which was funded by a NASA Early Career Initiative grant, will continue to flesh out the mission in the hope it might one day explore one of the more interesting planets in our solar system.

Learn More:
A. Gomez-Delrio et al -Design Considerations for Aerocapture Delivery of Uranus Orbiter and Probe
UT -Flexible Launch Opportunities for the Uranus Flagship Mission
UT -It's Time to Go Back to Uranus. What Questions do Scientists Have About the Ice Giants?
UT -Aerocapture is a Free Lunch in Space Exploration

Andy Tomaswick

Andy Tomaswick

Andy has been interested in space exploration ever since reading Pale Blue Dot in middle school. An engineer by training, he likes to focus on the practical challenges of space exploration, whether that's getting rid of perchlorates on Mars or making ultra-smooth mirrors to capture ever clearer data. When not writing or engineering things he can be found entertaining his wife, four children, six cats, and two dogs, or running in circles to stay in shape.