Testing time for MetOp Second Generation

Testing time for MetOp second generation
MetOp Second Generation's structural and thermal model during testing at ESA's ESTEC Test Centre in the Netherlands during summer 2019. Credit: ESA-SJM Photography

MetOp Second Generation (MetOp-SG) is a follow-on system to the successful MetOp satellites, the last of which launched into its 800 km polar orbit in 2018.

MetOp-SG is Europe's component of the Joint Polar System, which is a collaboration with the US. Eumetsat, the European Organisation for the Exploitation of Meteorological Satellites, operates the MetOp satellites and is responsible for developing the ground segment of the system and delivering the meteorological data to the world-wide user community. ESA is responsible for designing and manufacturing the space segment of the system—the satellites themselves.

For this campaign the test item was not flight hardware but a prototype version specially built for initial testing, known as the structural and thermal model (STM).

This initial MetOp-SG , standing 6.5m high and weighing in at 4.4 tonnes including propellant, was shaken, shocked and placed in prolonged vacuum under simulated sunlight to demonstrate the design's qualification for launch and readiness for space.

The MetOp Second Generation mission is actually made up of two different satellites each with different suites of instruments onboard.

Testing time for MetOp second generation
For MetOp Second Generation testing a prototype version specially built, known as the ‘structural and thermal model’ (STM). This MetOp-SG STM, standing 6.5m high and weighing in at 4.4 tons including propellant, was shaken, shocked and placed in prolonged vacuum under simulated sunlight to demonstrate the design’s qualification for launch and readiness for space. Credit: ESA-SJM Photography

"Our STM is actually a hybrid of these two satellite designs," explains Nick Goody, the mission's propulsion and assembly integration and testing engineer.

"The two satellites have a common platform, while the STM is equipped with the nadir-pointing instruments from satellite-A plus payload unit items from satellite-B, including amplifiers and power supplies. This hybrid configuration results in the maximum mass and power dissipation for the STM testing, intended for mechanical and thermal qualification. Those qualification objectives not covered by the STM will be addressed by the SAT-A and SAT-B proto-flight models."

The test campaign began at the Toulouse facility of Airbus Defence and Space in December 2018, where dummy units, thermal hardware and electrical harness was integrated, together with the propulsion module supplied by Airbus's facility in Stevenage, UK. This was followed by integration of test models of the instruments and the completion of its harness—the maze of wiring connecting everything together—and its multi-layer insulation wrapping.

"A micro-vibration test campaign was performed to characterize the transfer functions between the instruments and other microvibration exporters such as the reaction wheels," said MetOp-SG satellite engineering manager Enrico Corpaccioli.

"These measurements allow us to better analyze the effects of micro-vibrations on the instruments during the operation of the satellite when it is in orbit. Alignment measurements were also performed to provide a reference before environmental testing began."

Testing time for MetOp second generation
MetOp Second Generation's STM being mated with its propulsion module at the Toulouse facility of Airbus Defence and Space in December 2018. Credit: Airbus D&S

Then, in June 2019, the STM was transported to the ESTEC Test Centre in Noordwijk. The largest satellite test site in Europe, the center is equipped with facilities to simulate every aspect of the space environment under a single cleanroom roof.

Here it was unpacked for vibration testing. It was then filled with 760 kg of demineralized water, in place of the hydrazine propellant it will be fueled with before launch, for sine testing along each axis—undergoing a progressive sweep of frequencies and amplitudes to hunt out any potentially harmful structural resonances.

"Qualification levels are applied to the STM structure," adds Nick, "meaning that the amplitudes are significantly above the expected flight levels and the durations are longer in order to demonstrate the necessary margin in the design."

A quasi-static load test was also performed. Satellites are exposed to simultaneous static and dynamic loads during the launch phase due to launcher acceleration and aerodynamics. This quasi-static load test combines static and dynamic loads into an equivalent load which is applied to the satellite in a high amplitude sine burst over a few seconds.

A rocket launch is an extremely noisy event, so MetOp-SG was then transferred to the Large European Acoustic Facility. Here nitrogen is passed through massive acoustic horns within a sealed chamber, recreating the sound of a launch.

Testing time for MetOp second generation
MetOp-SG's STM was transported to the ESTEC Test Centre in a protective, air-conditioned container. Credit: ESA

The next step was a 'fit check' and separation test, involving mating the satellite with a launcher adapter provided by Arianespace, to guarantee the two designs fit together as intended and that the ring securing the satellite to the launcher—known as the clampband—operates correctly so that the separation can occur without any problem.

Next came the thermal test phase, which saw MetOp-SG moved into the Large Space Simulator, the largest vacuum chamber in Europe, equipped with a solar simulator based on an array of high power lamps.

A number of orbits were simulated in various hot and cold conditions until thermal stability was achieved within set levels. The results from this test allows experimental correlation of the spacecraft mathematical thermal model, used to verify the thermal control design.

Testing concluded with further alignment testing—to check the model had endured its test regime without structural deformation—and a leak check involving filling the propulsion module with helium gas.

"This test campaign has provided important qualification data," adds Nick, "allowing correlation of the models with representative data and confirming the analysis performed during the design stage. The structural thermal model has now been transported back to Toulouse in France, where the instrument models, propulsion module and dummy units are being removed.

  • Testing time for MetOp second generation
    MetOp-SG's STM on the Electrodynamic Shaker, used to simulate the intense vibrations of a space launch. In the background can be glimpsed part of another weather satellite, with the structural and thermal model of Meteosat Third Generation's Infrared Sounder instrument in the Large Space Simulator. Credit: ESA
  • Testing time for MetOp second generation
    MetOp-SG's structural and themal model being lowered into ESA's Large Space Simulator, the largest vacuum chamber in Europe, ahead of thermal vacuum testing during summer 2019. Credit: ESA-SJM Photography

"The satellite STM structure and propulsion module will be returned to their suppliers for refurbishment, as they are destined to be employed in MetOp SG-A's second flight model."

A tale of two MetOp-SGs

The two-satellite MetOp-SG system provides data from polar orbit for weather forecasting and climate monitoring and the suite of instruments provide information on atmospheric chemistry, air quality, oceanography, hydrology, wind, sea ice, precipitation and temperature profiles in the atmosphere.

MetOp SG-A hosts IASI-NG (Infrared Atmospheric Sounder Interferometer—New Generation) developed by French space agency CNES; the METimage advanced multispectral imaging radiometer developed by German Aerospace Center DLR; the ESA-developed Copernicus Sentinel-5 for atmospheric sounding plus ESA's MWS (Microwave Sounder); 3MI ((Multiview Multichannel Multipolarization Imager) and RO (Radio Occultation) instruments.

MetOp SG-B includes the same RO instruments as MetOp-SG-A plus the ESA-developed SCA (Scatterometer), ICI (Ice Cloud Imager), MWI (MicroWave Imager) and the CNES-contributed Argos Data Collection Service, collecting information from ocean-going buoys and a Space Environment Monitor contributed by Thales Alenia Space.

MetOp-SG is projected to enter service in 2023.


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