Crucial Data on Mars Landings Collected by Sensors During Successful Arrival of NASA’s Perseverance

MEDLI2 Hardware Mars 2020 Heat Shield

The MEDLI2 hardware is visible on the Mars 2020 heat shield as the heat shield falls toward the surface of Mars. The critical MEDLI2 electronics, two of the seven heat shield pressure transducers; measure the stagnation pressure during the hypersonic and supersonic phases of flight, and one of the 11 heat shield temperature locations can be seen. The copper-colored harness snaking around the heat shield is also evident. The circuitous path of the harness was to avoid the rover wheels and other items on the bottom of the rover. Credit: NASA/JPL-Caltech

MEDLI2 was one of the crucial technologies onboard the rover’s protective aeroshell that helped document the entry, descent, and landing of the spacecraft.

“Tango delta. Touchdown confirmed. Perseverance safely on the surface of Mars, ready to begin seeking the signs of past life.” For more than six years, the Mars Entry, Descent, and Landing Instrumentation 2 (MEDLI2) team waited to hear these words.

NASA’s Perseverance rover successfully landed on February 18, 2021, beginning its robotic exploration of the Red Planet. MEDLI2 was one of the crucial technologies on the rover’s protective aeroshell that helped document the entry, descent, and landing (EDL) of the spacecraft. All of the MEDLI2 data was stored on Perseverance for transmission to Earth after a successful landing.

MEDLI2 Operations Team

The MEDLI2 operations team in the control center at NASA’s Langley Research Center in Hampton, Virginia monitoring data received during the Perseverance’s final 5-hour coast to Mars. Credit: NASA

MEDLI2’s role was to collect critical data about the harsh environment during Perseverance’s entry through the planet’s atmosphere. It included three types of sensors – thermocouples, heat flux sensors, and pressure transducers – that measured extreme heat and pressure during entry. It also contained electronics and hardware for recording the thermal and pressure loads experienced during entry and through the parachute deployment.

MEDLI2 used its measurements to determine the heating and atmospheric forces that occurred on the heat shield and back shell. Together, these two components make up the aeroshell, which housed and protected the Perseverance rover during the cruise to Mars and EDL.

MEDLI2 was powered on five hours before the “7 Minutes of Terror,” or final 7-minute descent to Mars. This provided time for MEDLI2’s electronics to stabilize temperature and measure the initial conditions prior to entry. The team was relieved to receive the indication that MEDLI2 was successfully activated. The team continued to monitor the incoming data throughout this five-hour coast phase prior to entry.

The majority of the MEDLI2 sensors and the primary electronics were mounted on the Mars 2020 heat shield. About 10 seconds after the supersonic parachute deployed, MEDLI2 was powered down for the last time as it had completed its job. Since it is critical for the heat shield to be separated to allow the Perseverance rover to be extracted from the entry vehicle, it was required that MEDLI2 be turned off a few seconds before the separation to prevent any electrical power issues. The harness connecting the heat shield and back shell was then severed by the firing of a pyro-cutter, and the heat shield was dropped.

“We didn’t find any issues with the separation,” said Henry Wright, MEDLI2 project manager at NASA’s Langley Research Center in Hampton, Virginia. “The heat shield cleanly separated from the Mars 2020 entry vehicle. The MEDLI2 hardware was clearly visible on the heat shield as it fell toward the surface of Mars. Job well done!”

Perseverance also returned “critical event data” in real time during the EDL. It included a subset of the MEDLI2 data which allowed observations into what the entry vehicle was experiencing as the entry was happening. Three days after Perseverance’s successful landing, the remaining MEDLI2 data was transmitted back to Earth, and the next phase of the project began: data analysis and performance reconstruction.

“The returned data is fascinating. It’s like having a bird’s eye view of what’s happening to the aeroshell as it flies through Martian skies. The MEDLI2 sensor signals are so clear we could immediately pick out interesting phenomenon and crucial events” said Todd White, MEDLI2 principal investigator at NASA’s Ames Research Center in California’s Silicon Valley.

Data collected from MEDLI2 also provides measurements that will be used to determine the properties of the atmosphere the Mars 2020 entry vehicle flew through. MEDLI2 provides essential EDL observation data to understand how much margin remained on the Perseverance entry along with data that will be used to improve prediction models and tools for future missions.

Mars 2020 Entry Vehicle

Shown in this illustration: As the Mars 2020 entry vehicle slowed down, it performed various maneuvers to control its intended landing point. Eventually, the vehicle ejected six tungsten ballast masses to allow the vehicle to better align itself for deployment of its supersonic parachute. MEDLI2 used the new pressure transducers designed specifically for this final phase of flight. 1. The changes in surface pressure can be correlated to the various roll maneuvers performed by the Mars 2020 entry vehicle. 2. The ejection of the tungsten ballast masses and the change in surface pressure as the entry vehicle changes its attitude due to the shift in the entry vehicle’s center of mass. 3. The deployment of the supersonic parachute and the final deceleration prior to MEDLI2 being turned off. Credit: NASA/JPL-Caltech

Taking a Deeper Look Into the Data

Heat shield insulation temperatures were recorded throughout the complete entry phase and were consistent with the entry predictions. The peak measured temperature in the heat shield during the entry was 1,830 degrees Fahrenheit, or 1,000 degrees Celsius. That correlates to an estimated peak heat shield outer temperature of about 2,550 degrees Fahrenheit, or 1,400 degrees Celsius.

MEDLI2 also used its embedded thermocouples to determine how much of the heat shield protective insulation may have burned away or ablated. All of the thermocouples survived the entry heating pulse, indicating the heat shield ablation was very low. This observation could be used to reevaluate the amount of insulation that is needed on a heat shield to potentially reduce the overall entry vehicle mass.

MEDLI2 Data Complete Range of Environments

Data from MEDLI2 captured the complete range of environments experienced by the aeroshell protecting the Perseverance rover. Maximum conditions are experienced when the entry vehicle is traveling at about 20 times the speed of sound on Mars. 1. The current estimate of the maximum surface temperature of about 2500 degrees Fahrenheit. 2. The current estimate of the maximum surface pressure of about 4.2 psiA. 3. The change in the slope of the insulation temperature indicates an increase in the surface heat rate due to the change from laminar to turbulent flow. 4. The current estimate of the maximum back shell pressure due to the separated wake flow of about 0.05 psiA. 5. The current estimate of the total heat flux of about 3 to 5 W/cm2 due to the flow over the back shell and the heat radiated from the shock layer. Credit: NASA/JPL-Caltech

Surface pressures were also measured throughout the same phase with a peak surface pressure of the heat shield matching the team’s entry predictions. MEDLI2 picked different sensors to focus on accurately capturing different flight regimes. One sensor covered the complete range of the maximum surface pressures. The remaining six heat shield pressure measurements had a range to more accurately capture the conditions during the supersonic flight regime (from about five times the speed of sound on Mars through the deployment of the supersonic parachute). These sensors, combined with onboard inertial measurements, allow additional insight into how the entry vehicle performs when the impacts of atmospheric density variations and winds are more pronounced. The MEDLI2 pressure data will be used to improve the modeling approach for future EDL missions.

MEDLI2 included sensors on the back shell of the Mars 2020 entry vehicle, an area that until now has had limited observations. Surface pressure, insulation temperature, and direct surface heating measurements comprised the back shell sensor suite. Knowledge of the surface pressure on the back of the entry vehicle contributes to a reduction in the size of the landing footprint. Back shell insulation temperature data was within the initial predictions, which can be used to reduce the modeling uncertainty. As with the heat shield insulation, understanding the back shell insulation temperature performance could lead to a reduction in the back shell insulation mass. Direct surface heating measurements of the back shell also contribute to reducing the uncertainty in the predictive models.

MEDLI2 data also included a range of “housekeeping” measurements. These included a number of compensating temperature measurements of critical science sensors. Much of this housekeeping data is also of keen interest to the Mars 2020 team to aid in their own EDL reconstruction efforts. Part of the housekeeping measurements included sensors internal to the MEDLI2 support electronics (voltages, internal temperatures, MEDLI2 heartbeat/clock, etc.).

The MEDLI2 team will continue to analyze the data for the next six months, refining NASA’s understanding of the Mars atmosphere, the extreme conditions of entry, and how well the Mars 2020 aeroshell protected the rover. These lessons will be immediately useful for the next Mars missions, and even missions headed for Titan.

Langley led the MEDLI2 instrument development and project management. NASA’s Ames Research Center in California’s Silicon Valley and NASA’s Jet Propulsion Laboratory in Southern California contributed to MEDLI2. NASA’s Game Changing Development program within the Space Technology Mission Directorate funded the technology development.

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