Ætherion
ÆTHERION
Supersonic Experimental Rocket
SPECS
Length
Diameter
Mass
Motor
PRO75 - 3G Classic
Max. thrust
Apogee
Max. speed
G-Force
OVERVIEW
The Ætherion rocket represents a significant step in the field of experimental rocketry. Designed to achieve transonic and supersonic speeds, it aims to explore the aerodynamic behavior during the transition between these two flight regimes. This project builds on the experience gained from the Zéphir rocket and incorporates improvements for a more precise study of compressible fluid dynamics phenomena.
The Ætherion will be equipped with a PRO75 3G – Classic motor and an Aero-break system to control its maximum altitude, while ensuring a smooth landing thanks to a side-mounted parachute ejection system. To optimize flight stability, a StabTraj application has also been developed. The goal is to analyze shock waves, Prandtl-Meyer expansion fans, and oblique shocks, comparing experimental data with numerical simulations conducted using Ansys and SU2.
The results of this project will provide valuable insights for the design of future rockets, enhancing our understanding of supersonic flows and contributing to the advancement of cutting-edge flight technologies.
The Origins
Ætherion owes its origins to the Zéphir project, an former experimental rocket developed by Top Aero and launched in 2019 to test the basic principles of high-speed flight. Thanks to Zéphir, we gained a better understanding of the challenges of supersonic flight and in-flight stability. This experience has enabled us to make significant improvements to Ætherion, particularly in terms of aerodynamic design and management of the high pressures encountered during supersonic flight. Ætherion is therefore a natural evolution of Zéphir, incorporating the lessons learned and aiming to take its scientific approach even further.
The Origins
THE TEAM
OUR SPONSORS


