The satellite’s propulsion subsystem has been successfully prepared for fuelling and has undergone thorough system checks.
The check-out process was carried out by the OHB-Sweden team, who impressively managed to complete their tasks a full day ahead of schedule.
This time, the blog takes on a more technical angle, featuring insights from ESA Propulsion Expert Armin Herbertz. The propulsion subsystem consists of several meters of tubing, ensuring that the hydrazine propellant, stored in the 177-liter tank, reaches all eight thrusters. These thrusters are arranged in pairs at the four corners of the satellite. To regulate propellant flow and facilitate fuelling and pressurisation, the system incorporates multiple valves, including flow control valves, latching valves, and service valves.
Each thruster is safeguarded by two flow control valves positioned in series—both of which must be opened when the thruster is firing. For safety, these valves remain closed by default; unless powered, internal magnets keep them shut. The system is further divided into two thruster branches, each containing four thrusters, isolated from the main tank by latching valves. These bistable valves maintain their state—either open or closed—until actively switched, allowing controlled isolation or activation of an entire thruster branch.
At this stage, all valves have been rigorously checked for leaks. The leak testing process involves pressurising one side of a closed valve with helium while creating a vacuum on the downstream side. A helium detector then measures any traces of gas that pass through. Given the internal volume and surface area involved, these tests require considerable time and precision.
With the propulsion system successfully passing all checks, the satellite is now safeguarded against propellant loss once loaded, ensuring its readiness for propellant fuelling. While testing the propulsion subsystem is a meticulous and time-intensive task, it remains a crucial step in preparing for liftoff.
Next Week’s Preview: The Biomass satellite will undergo its final preparations, including the last MLI fitting, before being transferred to the hazardous processing facility for fueling operations. Stay tuned for more details in our next blog!
After the Abbreviated Functional Testing (AFT), the satellite has to be brought in vertical orientation, in order to proceed with the check-out of the propulsion system.
Blast shields are positioned around the Satellite, when the propulsion system is pressurized.
Congratulations to the OHB-Sweden team !
Leave a Reply