Purpose of the flight and payload description

This balloon mission was part of the qualification and testing phase of the parachute system for ExoMars (Exobiology on Mars) mission, an astrobiology programme by the European Space Agency (ESA) and the Russian space agency Roscosmos. The goals of ExoMars are to search for signs of past life on Mars, investigate how the Martian water and geochemical environment varies, investigate atmospheric trace gases and their sources and by doing so demonstrate the technologies for a future Mars sample-return mission. The first part of the programme was a mission launched in 2016 that placed the Trace Gas Orbiter into Mars orbit and released the Schiaparelli EDM lander. The orbiter is operational but the lander crashed on the planet's surface.

The second part of the programme was planned to launch in July 2020, when the Kazachok lander would have delivered the Rosalind Franklin rover on the surface, supporting a science mission that was expected to last into 2022 or beyond. The descent module requires two main parachutes -each with its own pilot chute for extraction- to help slow it down as it plunges through the martian atmosphere. The 15 meters-wide first stage main parachute will open while the descent module is still travelling at supersonic speeds, and the 35 meters-wide second stage main parachute is deployed once at subsonic speeds. Following separation of the parachutes, the speed must be suitable for the braking engines to safely deliver the landing platform and the rover onto the surface of Mars.

To test the performance of the parachutes before the flight, the UK-based company Vorticity Systems was selected as technical consultant under contract with Thales Alenia Space. A special capsule was built by the firm to perform the drop tests of the parachutes, first from low altitude using an helicopter and then from high altitude using a stratospheric balloon. These missions allowed to test the parachutes and deployment sequence with the same gravitational acceleration and atmospheric density as they will experience on Mars.

After the firsts series was completed in 2019 some anomalies were found on the descending system (see details below). As a result on March 2020, it was announced that the second mission was being delayed to 2022 as a result of the problems with the parachutes, which could not be resolved in time for the launch window. After studying the problem and some modifications, a new series of parachute tests were needed which were performed in Oregon during 2020 and from Sweden in 2021.

Details of the balloon flight

Balloon launched on: 5/28/2019 at 2:56 utc
Launch site: European Space Range, Kiruna, Sweden  
Balloon launched by: Swedish Space Corporation (SSC)
Balloon manufacturer/size/composition: Zero Pressure Balloon Raven SF4 - 113.000 m3
End of flight (L for landing time, W for last contact, otherwise termination time): 5/28/2019
Balloon flight duration (F: time at float only, otherwise total flight time in d:days / h:hours or m:minutes - ):  
Payload weight: 800 kgs

The first high altitude test took place on May 28, 2019 to test the deployment sequence of all four parachutes. The balloon was launched from ESRANGE at 2:56 utc and after a nominal ascent the dummy re-entry body was released from an altitude of 29 km. Shortly after the first pyrotechnic mortar activated normally to release the first pilot chute - which inflated correctly. The main parachute lid release mechanism worked and the first main parachute also inflated well, but several radial tears in the fabric were observed immediately following extraction from the main parachute bag, before the parachute experienced maximum load. The second pyrotechnic mortar also worked normally, ejecting the second pilot chute, which also inflated as expected. The second main parachute was extracted from its bag, but one radial tear was observed, again before reaching peak inflation loads.

All the data onboard the drop test vehicle were recovered and analysed. These data included acceleration, angular rates, magnetometer, GPS, and barometer data, together with camera footage.

Detailed analysis of the telemetry parameters recorded during the test confirmed that a good level of the expected aerodynamic drag was nevertheless achieved in spite of the parachute tears. The overall descent time of the entire test was also close to prediction. The second parachute was quickly recovered and examined while it took a few days to identify and recover the first parachute that had travelled over 100 km following separation.

External references

Images of the mission


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