ESA title
Understanding how particles emitted during launch affect the environment
Enabling & Support

Understanding how particles emitted during launch affect the environment

06/05/2022 75 views 0 likes
ESA / Enabling & Support / Space Engineering & Technology / Shaping the Future

The ESA-EMAP activity is dedicated to the experimental modelling of alumina particulates in solid boosters. This  requirement is rooted in the uncertainty regarding the impact of the alumina particles emitted by the solid rocket motors (SRMs) of European launch systems on the ozone depletion in the stratosphere.

This uncertainty needs to be addressed, in particular when facing the significantly increased number of rocket launchers predicted in the new space era.

ESA-EMAP has focused on an experimental investigation into how the particles form, as well as better understanding how they flow and move (and subsequently what impact they can have on the stratosphere). Conducted by DLR, Germany, with the TDE, the model will help improve knowledge about the alumina particles (size distribution, crystalline nature, etc) present in European solid rocket motors to support more accurate environmental assessments of Europe’s launches.

ESA-EMAP activity is dedicated to the experimental modelling of alumina particulates in solid boosters
ESA-EMAP activity is dedicated to the experimental modelling of alumina particulates in solid boosters

The tests were executed with a solid rocket motor (SRM) mimicking a launch system and operating under flight-realistic conditions by placing a rocket motor into a wind tunnel. The particle formation was assessed from the combustion chamber throughout the nozzle to its final state, as it would be expected in the atmosphere.

The activity developed and recorded a vast database on solid rocket exhaust plumes. The database now includes information on how the particles moved, their path along three different planes, particle size, velocity, temperature distribution, and the gas composition of the plume. That database now provides a foundation for further analytical explorations and the opportunity to validate models associated with the physics of solid rocket exhaust plumes.

T418-408MP closed in 2021.