310 kgf rocket engine CFD
Chamber pressure - 27 bar
Nozzle exit pressure - bar
90% H2O2 Kerosene
Software - SolidWorks 2016 FlowSimulation
For URAN 1 rocket.
2 years ago 00:10:49 1
3 years ago 00:09:37 5
4 years ago 00:01:04 100
13 years ago 00:00:37 13
