-
Notifications
You must be signed in to change notification settings - Fork 0
Home
XavBell edited this page Apr 8, 2022
·
2 revisions
Currently, all the measure entered for the engine is used to calculate the mass, none of those values is used for engine thrust. Engine thrust is entered manually, along with mass rate. The quantity of fuel and oxidizer you enter will determine run time, considering flow rate. If your ratio is not good, it will become unused fuel/oxidizer. If at the end of the simulation you obtain negative values it means that your rocket is not powerful enough or it's an impossible case. Currently, aerodynamics forces is not calculated.
- Create propellants tanks with a defined material with a precise size.
- Save and share your rockets.
- Create engines according to a lot of parameters.
- Simulate rocket launch.
- Full roadmap