Tag Archives: descent module

Experimental investigation of aero-thermodynamic characteristics of “ExoMars” project descent module at hypersonic velocities.

High-Speed Missions and Vehicles, HiSST 2018, Hypersonic Aerodynamics, Testing and Evaluation, Thermal and Energy Management Systems, Thermal Protection SystemsBy tvermin October 6, 2023

Drozdov S.M., Brazhko V.N., Davletkildeev R.A., Fedorov D.S., Shemetov I.M.

DOI Number XXX-YYY-ZZZ
Conference Number HiSST 2018_640799