‘7 Minutes of Terror’: The Technology Perseverance Will Need to Survive Landing on Mars

This month has been a busy one for Mars exploration. Several countries sent missions to the red planet in June last year, taking advantage of a launch window. Most have now arrived after their eight-month voyage.

Within the next few days, NASA will perform a direct entry of the Martian atmosphere to land the Perseverance rover in Mars’s Jezero Crater.

Perseverance, about the size of a car, is the largest Mars payload ever—it literally weighs a ton (on Earth). After landing, the rover will search for signs of ancient life and gather samples to eventually be returned to Earth.

The mission will use similar hardware to that of the 2012 Mars Science Laboratory (MSL) mission, which landed the Curiosity rover, but will have certain upgrades including improved rover landing accuracy.

Curiosity’s voyage provided a wealth of information about what kind of environment Mars 2020 might face and what technology it would need to survive.

An artist’s impression of Mars 2020 approaching the red planet. NASA/JPL-Caltech

Mars: a Most Alien Land

As Mars is a hostile and remote environment with an atmosphere about 100 times thinner than Earth’s, there’s little atmosphere for incoming spacecraft to use to slow down aerodynamically.

Rather, surviving entry to Mars requires a creative mix of aerodynamics, parachutes, retropropulsion (using engine thrust to decelerate for landing), and often a large airbag.

Also, models of Martian weather aren’t updated in real time, so we don’t know exactly what environment a probe will face during entry. Unpredictable weather events, especially dust storms, are one reason landing accuracy has suffered in previous missions.

NASA engineers call the entry, descent, and landing phase (EDL) of Mars entry missions the “seven minutes of terror.” In just seven minutes there are myriad ways entry can fail.

A profile of Mars 2020’s entry, descent and landing phase. NASA JPL

Thermal Protection

The 2012 MSL spacecraft was fitted with a 4.5-meter-diameter heat shield that protected the vehicle during its descent through Mars’s atmosphere.

It entered the Martian atmosphere at around 5,900m per second. This is hypersonic, which means it’s more than five times the speed of sound.

Mars 2020 will be similar. It will rely heavily on its thermal protection system, including a front heat shield and backshell heat shield, to stop hot flow from damaging the rover stowed inside.

Pictured are the Mars 2020 backshell heat shield (foreground) and the main PICA heat shield (background). NASA/JPL-Caltech

At hypersonic speeds, Mars’s atmosphere won’t be able to get out of the spacecraft’s way fast enough. As a result, a strong shock wave will form off the front.

In this case, gas in front of the vehicle will be rapidly compressed, causing a huge jump in pressure and temperature between the shock wave and the heat shield.

The hot post-shock flow heats up the surface of the heat shield during the entry, but the heat shield protects the internal structure from this heat.

Since the MSL 2012 and Mars 2020 missions use relatively larger payloads, these spacecrafts are at higher risk of overheating during the entry phase.

But MSL effectively circumvented this issue, largely thanks to a specially-designed heat shield which was the first Mars vehicle ever to make use of NASA’s Phenolic Impregnated Carbon Ablator (PICA) material.

This material, which the Mars 2020 spacecraft also uses, is made of chopped carbon-fiber embedded in a synthetic resin. It’s very light, can absorb immense heat, and is an effective insulator.

Guided Entry

All entries before the 2012 MSL mission had been unguided, meaning they weren’t controlled in real-time by a flight computer.

Instead, the spacecraft were designed to hit Mars’s “entry interface” (125km above the ground) in a particular way, before landing wherever the Martian winds took them. With this came significant landing uncertainty.


The area of landing uncertainty is called the landing ellipse. NASA’s 1970s Viking Mars missions had an estimated landing ellipse of 280x100km. But both MSL and now Mars 2020 were built to outperform previous efforts.

The MSL mission was the first guided Mars entry. An upgraded version of the Apollo guidance computer was used to control the vehicle in real time to ensure an accurate landing.

With this, MSL reduced its estimated landing ellipse to 20×6.5km and ended up landing just 2km from its target. With any luck, Mars 2020 will achieve similar results.

Pictured are NASA’s various Mars landing sites, including the proposed Perseverance landing site. Perseverance is expected to land in a relatively less clear area. NASA/JPL-Caltech

Supersonic Parachuting

A parachute will be used to slow down the Mars 2020 spacecraft enough for final landing maneuvers to be performed. With a 21.5m diameter, the parachute will be the largest ever used on Mars and will have to be deployed faster than the speed of sound.

Deploying the parachute at the right time will be critical for achieving an accurate landing. A brand new technology called “range trigger” will control the parachute’s deployment time, based on the spacecraft’s relative position to its desired landing spot.

State-of-the-Art Navigation

About 20 seconds after the parachute opens, the heat shield will separate from the spacecraft, exposing Perseverance to the Martian environment. Its cameras and sensors can begin to collect information as it approaches ground.

The rover’s specialized terrain-relative navigation system will help it land safely by diverting it to a stable landing surface.

Perseverance will compare a pre-loaded map of the landing site with images collected during its rapid descent. It should then be able to identify landmarks below and estimate its relative position to the ground to an accuracy of about 40m.

Terrain-relative navigation is far superior to methods used for past Mars entries. Older spacecraft had to rely on their own internal estimates of their location during entry.

And there was no way to effectively recalibrate this information. They could only guess where they were to an accuracy of about 2-3km as they approached ground.

The Final Touchdown

The parachute carrying the Mars 2020 spacecraft can only slow it down to about 320km per hour.

To land safely, the spacecraft will jettison the parachute and backshell and use rockets facing the ground to ease down for the final 2,100m. This is called “retropropulsion.”

And to avoid using airbags to land the rover (as was done in missions prior to MSL), Mars 2020 will use the “skycrane” maneuver; a set of cables will slowly lower Perseverance to the ground as it prepares for autonomous operation.

Once Perseverance senses its wheels are safely on the ground, it will cut the cables connected to the descent vehicle (which will fly off and crash somewhere in the distance).

And with that, the seven minutes of terror will be over.The Conversation

Perseverance rover being placed on Martian soil by the skycrane. NASA/JPL-Caltech

This article is republished from The Conversation under a Creative Commons license. Read the original article.

Image Credit: NASA/JPL-Caltech

Chris James
Chris Jameshttps://researchers.uq.edu.au/researcher/16430
Chris' research is primarily related to experimental hypersonics. His research interests include expansion tube and shock tunnel test facility design and condition development and the experimental study of planetary entry aerothermodynamics using both optical techniques and physical measurements. Chris has authored and co-authored 21 journal publications and 40 conference publications in his field. Chris is an ARC DECRA Fellow in the Centre for Hypersonics in the School of Mechanical and Mining Engineering at the University of Queensland (UQ). Chris graduated from a Mechanical Engineering degree at UQ in 2012. Following this, he completed his PhD in the Centre for Hypersonics. During his PhD he developed very high speed Uranus and Saturn entry test conditions which were used to perform the fastest experiments which have ever been performed in an expansion tube, as well as developing expansion tube simulation and analysis codes which are now widely used in the Centre for Hypersonics. During his PhD he also enrolled in a cotutelle program with École Centrale Paris in Paris, France, and after being awarded an Eiffel Scholarship by the French government, he passed a year on exchange in Paris, France. In France, Chris was working on developing the capability to perform radiating simulations to support his experimental work at UQ. Post PhD he was employed in the Centre for Hypersonics helping to develop the X3R reflected shock tunnel, while also supervising and conducting expansion tube research on the X2 expansion tube at UQ. Chris became a Lecturer at the start of 2020 and was also rewarded an Australian Research Council DECRA early career fellowship to study Mars return conditions with heated test models at UQ over the next several years. He was the 2020 recipient of the UQ EAIT Faculty Early Career Researcher Award. Chris lectures both hypersonics and space engineering, covering varied topics such as high temperature gas dynamics, orbital mechanics, rocket trajectories, spacecraft design, spacecraft thermal and power management, and planetary entry.
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