ORBITS · PROPULSION · TRANSFERS
Draw the journey
to another planet.
Estimate a Hohmann trajectory from Earth orbit, its delta-v and the required propellant mass.
TRAJECTORY ANALYSIS
Terre → Mars
Estimate ready
TRANSFER MAP
Travel window
Earth orbitTarget orbitSun
BREAKDOWN
Key figures
How to read these results?
The delta-v is the change in velocity to be provided. The propellant mass is estimated using the Tsiolkovsky equation, based on the entered dry mass and specific impulse.